The content of accreditation studies of calibration laboratories.
\r\n\t
",isbn:"978-1-80356-495-1",printIsbn:"978-1-80356-494-4",pdfIsbn:"978-1-80356-496-8",doi:null,price:0,priceEur:0,priceUsd:0,slug:null,numberOfPages:0,isOpenForSubmission:!0,isSalesforceBook:!1,hash:"2d409a285bea682efb34a817b0651aba",bookSignature:"Dr. Saeed El-Ashram, Dr. Guillermo Téllez and Dr. Firas Alali",publishedDate:null,coverURL:"https://cdn.intechopen.com/books/images_new/11635.jpg",keywords:"PCR, Genotyping, ELISA, Cell Lines, 2D Culture, 3D Culture, PRRs, CD4 Responses, CD8 Responses, Behavior Manipulation, Parasite Cysts, Psychiatric Disorders",numberOfDownloads:null,numberOfWosCitations:0,numberOfCrossrefCitations:null,numberOfDimensionsCitations:null,numberOfTotalCitations:null,isAvailableForWebshopOrdering:!0,dateEndFirstStepPublish:"March 4th 2022",dateEndSecondStepPublish:"May 6th 2022",dateEndThirdStepPublish:"July 5th 2022",dateEndFourthStepPublish:"September 23rd 2022",dateEndFifthStepPublish:"November 22nd 2022",remainingDaysToSecondStep:"16 days",secondStepPassed:!0,currentStepOfPublishingProcess:3,editedByType:null,kuFlag:!1,biosketch:"Dr. El-Ashram's research focuses on apicomplexan parasites, such as Toxoplasma and Eimeria. 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The overall target of his research is to provide information that will aid in the design of novel therapeutic strategies aimed at the prevention and/or treatment of these complicated infections. To achieve this objective, they are utilizing new technology, including Proteomics, Immunoproteomics, Mass Spectrometry, Next Generation Sequencing, Tetramers, Real-time PCR, Immunohistochemistry and Bioinformatic and Flow Cytometry Analyses to dissect the host-pathogen interactions in single or combined infections. Dr. El-Ashram's laboratory deciphers the formation and evolution of host specialization in the foodborne illnesses, such as Salmonella spp., Clostridium perfringens, Campylobacter jejuni and Bacillus cereus by building a genome-based phylogeny and studying the Whole genome sequencing (WGS) as an effective and rapid surveillance tool of foodborne disease.",institutionString:"Foshan University",position:null,outsideEditionCount:0,totalCites:0,totalAuthoredChapters:"0",totalChapterViews:"0",totalEditedBooks:"0",institution:{name:"Foshan University",institutionURL:null,country:{name:"China"}}}],coeditorOne:{id:"73465",title:"Dr.",name:"Guillermo",middleName:null,surname:"Téllez",slug:"guillermo-tellez",fullName:"Guillermo Téllez",profilePictureURL:"https://mts.intechopen.com/storage/users/73465/images/system/73465.jpg",biography:"Guillermo Tellez-Isaias was born in Mexico City, in 1963. 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In shortly, by the biomedical calibration measurements, it is established whether the medical devices are appropriate to the international standards or not, and the problems are also determined if the device is not adequate to the international standards (Sezdi, 2012).
\n\t\t\tBiomedical calibration measurement is different from other industrial calibration studies. Measurements are generally performed where the medical device that will be tested, is used in hospital. Only some medical devices, for example pipettes, thermometers are tested in laboratory environment.
\n\t\t\tAccreditation is the appraising of a measurement service in according to the international technical criterias, is the acception of its qualification and the controlling of it regularly. For an enterprise, being accredited is a reputable status. It shows that the enterprise has a quality management system and performs the requirements of the implemented standards. The enterprices are periodically recontrolled by an accreditation agency to protect the status and to continue fulfilling of the requirements of the business standards. The controls create the most important quality assurance of the businesses that take service from these laboratories.
\n\t\t\tIn many countries, from Brazilia to China, there are accreditation studies (Boldyrev et al., 2004; Boschung et al., 2001; Iglicki et al., 2006; Kartha et al., 2003; Alexander et al., 2008; Goff et al., 2009; McGrowder et al., 2010). In Turkey, the studies of accreditation is controlled by Turkish Accreditation Agency (TURKAK). If the list of the accredited laboratory is investigated from the web site of TURKAK, it is seen that there are approximately 14 accredited enterprises that give services in biomedical calibration measurements (TURKAK website). But these are not in a single accredited enterprise type. While some of them are accepted as testing laboratories, some of them are accepted as calibration laboratories, the others are accepted as inspection bodies.
\n\t\t\tThe standard used in the accreditation of testing laboratories and calibration laboratories is TS EN ISO/IEC 17025:2005. ISO 17025 contains the quality management system of the testing and calibration laboratory. It examines all work flows, organization structure and technical suffiency. The standard used in the accreditation of inspection bodies is TS EN ISO/IEC 17020:2004 (ISO IEC 17025, 2005; ISO IEC 17020, 2004).
\n\t\t\tThere is not yet a specific study about the medical accreditaton in TURKAK. If hospitals demand the medical accreditation during they take the medical calibration service, they must work with the accredited laboratory in according to their measured medical device or system. It can be a medical device, radiological system or only a parameter such as temperature, mass…etc. There is a confusion about which accreditation studies should preferred for which medical devices. Is the accreditation certificate about non-medical parameters sufficient technically for biomedical calibration? In other words, is testing of a defibrilator by the mass accreditation or testing of an anesthetic machine by the temperature accreditation, ethical?
\n\t\t\tThere may be many parameters that must be considered during the biomedical calibration measurements of any medical device. For example, testing of a ventilator contains flow, pressure and volume parameters. If a sufficieny is wanted, sufficiency about three parameters must be wanted seperately. In addition to this, the personnel who will perform the measurement, must be professional. The biomedical calibration needs the specialization of the biomedical personnel. It brings many problems that the biomedical calibration is performed by the non-educated personnel about biomedical and that the industrial accreditation is accepted as sufficient. Particularly, inattentive studies, in operation rooms and intensive care rooms, causes many unexpected problems.
\n\t\t\tThe important point that attracts the attention in this study is that the hospitals take the inadequate services if they don’t investigate the accreditation content. If the content of the accreditation studies is known, the customer will be knowledgeable about which accreditation should be preferred for which medical device or medical system.
\n\t\tAccreditation is a quality infrastructure tool which supports the credibility and value of the work carried out by conformity assessment bodies. Accreditation provides formal recognition that an organisation is meeting internationally accepted standards of quality, performance, technical expertise, and competence.
\n\t\t\tA product or service accompanied by a conformity attestation delivered by an accredited conformity assessment body inspires trust as to the compliance with applicable specified requirements. Thereby accreditation favours the elimination of technical barriers to trade. Accreditation provides a global acceptance of the services and establishs a confidence for the quality.
\n\t\t\tThe trusting mechanism between accreditation bodies is constructed on the multi literal agreements at the international and regional accreditation body organisations, like IAF ( International Accreditation Forum), ILAC (International Laboratory Accreditation Cooperation), EA (Europen Cooperation for Accreditation), etc.
\n\t\t\tTurkish Accreditation Agency (TURKAK) started to provide accrediation services in 2001 and became a cooperator of Europian Cooperation for Accreditation (EA) for all available accreditation schemes at 2008. Currently TURKAK is a full member of EA, IAF and ILAC. It serves as international accreditation agency.
\n\t\t\tAccreditation is beneficial to the accredited body itself, to Government and to users of accredited bodies.
\n\t\t\tAccredited bodies have benefits as below:
\n\t\t\tthe laboratories are controlled by independent conformity assessment bodies and they meet international standards for competence,
an effective marketing tool is provided,
the measurements are demonstrated as traceble in according to the national or international standards,
Accredited service provides benefits for customers:
\n\t\t\tassurance that tests are performed by using calibrated equipment by personnel with the right level of expertise,
assurance that calibration or test devices are controlled and traced periodically in according to the international standards,
elimination of technical barriers to trade,
addition of credibility to the test results by accredited conformity assessment bodies,
Generally, accreditation applications are classified as 4 items.
\n\t\t\tAccreditation of testing, calibration and medical laboratories,
accreditation of product, service or inspection,
accreditation of certification of management systems, and
accreditation of personal certification bodies.
In laboratory and inspection accreditation, high respectability both at the national and international level as an indicator of technical competence is essential. Laboratory and inspection accreditation aim to give services accurate and reliable testing, analysis or calibration measurements. Laboratory accreditation ensures the official recognition of laboratory competence and offers an easy method to customers in determining and choosing reliable testing, analysis and calibration services.
\n\t\t\tThe process of laboratory accreditation is regulated and standardized according to the international standards. Reports and certificates issued by accredited laboratories are internationally accepted. While the standard for testing and calibration laboratories is ISO IEC 17025:2005, the standard for inspection bodies is ISO IEC 17020:2004.
\n\t\t\tAccreditation activities of certification bodies of management system provide quality of certification of management system. Accreditation services in this field is generally given for ISO 9001:2008 certification, ISO 14001:2004 certification, ISO 22000:2005 certification, ISO 27001:2005 certification and ISO 13485:2003 certification. For this type of accreditation, ISO/IEC 17021:2011 standard is used (ISO/IEC 17021, 2011).
\n\t\t\tAccreditation of personal certification bodies that certificate the personnel making conformity assessments to make their activities in accordance with specified national and international standards, is provided by using the standard of ISO/IEC 17024:2003 (ISO/IEC 17024, 2003).
\n\t\t\tAccreditation bodies use accreditation mark or logo over their certificates or reports that contain their measurement/test results. But, such logo or marks must be used only over the certificates or reports including accredited facilities. TURKAK also provides accreditation symbol to be used in the output documents to be issued for the accredited services. It contains information about the accreditation field, accreditation standard and unique number of the accredited body, the accreditation number. The logo used by TURKAK can be seen in figure 1.
\n\t\t\tThe accreditation logo used by TURKAK (TURKAK website).
For accreditation studies, the quality assurance of the test results is obtained by interlaboratory comparisons and proficiency testing (PT) (Bode, 2008; Kubota et al., 2008; Kopler et al., 2005). The interlaboratory comparisons and proficiency testing bring significant benefits to laboratories.
\n\t\t\t\tProficiency Testing provides the infrastructure for a laboratory to monitor and improve the quality of its routine measurements (fig. 2). Proficiency Testing is the only quality measure which is specifically concerned with a laboratory’s outputs. Proficiency Testing gives a possibility to identify any problems caused from other aspects of its quality system, such as staff training and method validation.
\n\t\t\t\tThe factors in accreditation process.
Proficiency Testing is treated as important performance criteria regarding the evaluation of the technical competence of the laboratories. Laboratories that will be accredited should participate to Proficiency Testing programme or/and interlaboratory comparison for the main and sub disciplines they demand for accreditation and should submit satisfactory results according to defined criterias.
\n\t\t\t\tProficiency Testing providers demonstrate the quality of their Proficiency Testing programmes. There are two important international guides to which Proficiency Testing providers can demonstrate the quality of their Proficiency Testing programmes:
\n\t\t\t\tISO/IEC 17043: Conformity assessment - General requirements for proficiency testing (ISO/IEC 17043, 2007)
ILAC G13: Guidelines for the Requirements for the Competence of Providers of Proficiency Testing Schemes (ILAC G13, 2007)
The basic of the ISO/IEC 17043 is the ISO/IEC Guide 43. For several years, this document has provided several guidance on the development and operation laboratory proficiency testing for a relatively new field of activity. It contained very basic guidance and little attention to the use of the outcomes by laboratory accreditation bodies (Tholen, 2007).
\n\t\t\t\tGuide 43 have provided guidance in 5 areas (ISO Guide 43, 1997). They are;
\n\t\t\t\tto distinguish between use of interlaboratory comparisons for Proficiency Testing and for other purposes (introduction to Part 1)
the development and operation of Proficiency Testing schemes (Part 1)
the selection and the use of schemes by laboratory accreditation bodies (Part 2)
guidance on statistical methods (Annex A) and
guidelines for development of a quality manual for the operation of Proficiency Testing schemes (Annex B)
The statistical annex led to the development of ILAC Guide 13. ILAC G13 contains the technical guidelines from Guide 43-1 expressed as requirements and includes the quality management system requirements from ISO/IEC Guide 25. Since G13 has management system requirements that are consistent with ISO/IEC 17025, Proficiency Testing providers accredited to this document are considered to be in conformity with the requirements of ISO 9001:2000 (Tholen, 2007). The standard ISO/IEC 17043 describes the criteria concerning the quality to be respected when developing proficiency tests and the use that can be made of these tests by the accreditation bodies. ILAC-G13 is useful to organizers for competence (Fraville et al., 2010).
\n\t\t\t\tThe Proficiency Testing programmes of many Proficiency Testing providers around the world are now accredited by their national accreditation bodies, normally against the above documents. However, not all countries are ready to accredit Proficiency Testing providers, and not all Proficiency Testing providers wish to be accredited.
\n\t\t\t\tProficiency Testing programmes are operated by a variety of organizations within Europe and the rest of the world. Many Proficiency Testing programmes are international. There is a database of available Proficiency Testing programmes. In selecting the most appropriate Proficiency Testing it is important to consider a number of issues in order to judge its suitability for your purpose (ISO Guide 34, 2000; ISO Guide 43, 1997).
\n\t\t\tThe accreditation standards used in biomedical calibration measurements can be classified into 2 groups. TS EN ISO / IEC 17025 and TS EN ISO / IEC 17020. While the standard of 17025 is used for the accreditation of testing and calibration laboratories, the standard of 17020 is used for the accreditation of inspection bodies.
\n\t\t\tThe laboratory accreditation standards should not be confused with ISO 9001 standard. ISO 9001 is widely used in the assessment of the quality systems of production and service organizations. Certification of organizations according to the ISO 9001 system expresses the compliance of that organization\'s quality system with this standard (ISO 9001). When certifying laboratories according to ISO 9001, this certification makes no statement on the technical competence of laboratories. From this point, the certificate\'s power to convince the market and prospects of laboratories is quiet insufficient.
\n\t\t\tISO IEC 17025, entitled “General Requirements for the Competence of Testing and Calibration Laboratories”, is an international standard describing the general requirements to meet for the recognition of that a laboratory is competent to perform specific tests (ISO IEC 17025; 2005). This international standard is used to develop the quality, management and technical systems of laboratories (Abdel-Fatah, 2010; Glavic-Cindro et al., 2006; Brantner et al., 2011; Zapata-Garcia et al., 2007; Jerone et al., 2008). Technical requirements are updated to include the addition of formal personnel training plans and detailed records, method development and validation procedures, measurement of method uncertainty, and a defined equipment calibration and maintenance program (Honsa et al., 2003). ISO 17025 certification can be applied to all organizations that give services of testing or calibration. These organizations are the first-party, second-party and third-party laboratories.
\n\t\t\t\tFirst–party Laboratories: Manufacturer Laboratories, Second-party Laboratories: Customer Laboratories, Third-party Laboratories: Independent Laboratories.
\n\t\t\t\tThis standard can be applied to all laboratories regardless of the scope of test or calibration activities and the number of personnel.
\n\t\t\t\tIf testing and calibration laboratories comply with the requirements of this standard, a quality management system to meet the principles of ISO 9001 will be also applied. There is a cross-match among TS EN ISO 17025 standard and ISO 9001. TS EN ISO 17025 standard covers technical competence requirements, not covered by ISO 9001.
\n\t\t\t\tTS EN ISO 17025 standard is assessed in two main categories. The standard of TS EN ISO IEC 17025 contains both the management and technical requirements. In standard, 4th item describes the management system and 5th item describes the technical activities. The content of 17025 standard is as follows:
\n\t\t\t\t\t0 Introduction
\n\t\t\t\t\t1 Scope
\n\t\t\t\t\t2 Cited in standards and / or documents
\n\t\t\t\t\t3 Terms and definitions
\n\t\t\t\t\t4 Management requirements
\n\t\t\t\t\t4.1 Organization
\n\t\t\t\t\t4.2 Management system
\n\t\t\t\t\t4.3 Document control
\n\t\t\t\t\t4.4 Review of requests, tenders and contracts
\n\t\t\t\t\t4.5 Subcontracting of tests and calibrations
\n\t\t\t\t\t4.6 Purchasing of service and materials
\n\t\t\t\t\t4.7 Customer service 4.8 Complaints
\n\t\t\t\t\t4.8 Complaints
\n\t\t\t\t\t4.9 Control of nonconforming testing and / or calibration work
\n\t\t\t\t\t4.10 Improvement
\n\t\t\t\t\t4.11 Corrective action
\n\t\t\t\t\t4.12 Preventive action
\n\t\t\t\t\t4.13 Control of records
\n\t\t\t\t\t4.14 Internal controls
\n\t\t\t\t\t4.15 Management reviews
\n\t\t\t\t\t5 Technical requirements
\n\t\t\t\t\t5.1 General
\n\t\t\t\t\t5.2 Personnel
\n\t\t\t\t\t5.3 Accommodation and environmental conditions
\n\t\t\t\t\t5.4 Test and calibration methods and method validation
\n\t\t\t\t\t5.5 Devices
\n\t\t\t\t\t5.6 Measurement traceability
\n\t\t\t\t\t5.7 Sampling
\n\t\t\t\t\t5.8 Calibration procedures
\n\t\t\t\t\t5.9 Assuring the quality of test and calibration results
\n\t\t\t\t\t5.10 Reporting of the results
\n\t\t\t\t\tThe laboratory must be an institution that can be held legally responsible. Laboratory management system must consist of facilities in fixed laboratory and temporary or mobile facilities that are linked to the laboratory.
\n\t\t\t\tISO 17020, entitled “General Criteria for the Operation of Various Types of Bodies Performing Inspection”, is an internationally recognized standard for the competence of inspection bodies. Inspection parameters may include such aspects as the quantity, quality, safety, suitability, facilities or systems (ISO IEC 17020; 2004).
\n\t\t\t\tThere are 3 types of inspection organizations. They are:
\n\t\t\t\tTS EN ISO 17020 standard can be applied regardless of the scope of inspection activities in the company. TS EN ISO 17020 certification can be given all kinds of inspection bodies that are willing to give service in accordance with this standard.
\n\t\t\t\tIn the standard of TS EN ISO IEC 17020, the technical requirements are the main aspect. TS EN ISO 17020 standard consists of 16 items. They are:
\n\t\t\t\t\t0 Introduction
\n\t\t\t\t\t1 Scope
\n\t\t\t\t\t2 Definitions
\n\t\t\t\t\t3 Administrative Rules
\n\t\t\t\t\t4 Independence, impartiality and integrity
\n\t\t\t\t\t5 Privacy
\n\t\t\t\t\t6 Organization and management
\n\t\t\t\t\t7 Quality System
\n\t\t\t\t\t8 Personnel
\n\t\t\t\t\t9 Equipment
\n\t\t\t\t\t10 Inspection methods and procedures
\n\t\t\t\t\t11 Samples and materials to be inspected
\n\t\t\t\t\t12 Records
\n\t\t\t\t\t13 Inspection reports and inspection certificates
\n\t\t\t\t\t14 The use of subcontractors
\n\t\t\t\t\t15 Complaints and appeals
\n\t\t\t\t\t16 Co-operation
\n\t\t\t\tAs it was mentioned earlier, there are 3 accreditation types for biomedical calibration measurements. They are:
\n\t\t\tCalibration laboratories
Testing laboratories
Inspection bodies
A calibration laboratory is a laboratory that performs test, calibration and repair of measuring instruments. The calibration of equipment is achieved by means of a direct comparison against measurement standards or certified reference materials. These standards are also regularly calibrated themselves, in comparison with another standard of lower uncertainty.
\n\t\t\t\tPressure | \n\t\t\t\t\t\t\t0 - 70 bar | \n\t\t\t\t\t\t\tAir | \n\t\t\t\t\t\t\t0,2 % | \n\t\t\t\t\t\t\tEuramet CG-17 / v.01 | \n\t\t\t\t\t\t
70 - 700 bar | \n\t\t\t\t\t\t\tHydraulic | \n\t\t\t\t\t\t\t0,2 % | \n\t\t\t\t\t\t||
Temperature distribution of controlled volume | \n\t\t\t\t\t\t\t-40 +200 oC | \n\t\t\t\t\t\t\tIn controlled volume (oven, incubator, freezer….) | \n\t\t\t\t\t\t\t0,68 oC | \n\t\t\t\t\t\t\tEuramet CG-13 / v.01 | \n\t\t\t\t\t\t
Scales (non automatic) | \n\t\t\t\t\t\t\t0 – 600 gr | \n\t\t\t\t\t\t\tE2 class mass | \n\t\t\t\t\t\t\t2 10-6\n\t\t\t\t\t\t\t | \n\t\t\t\t\t\t\tEuramet CG-18 / v.03 | \n\t\t\t\t\t\t
0 – 10 kg | \n\t\t\t\t\t\t\tF1 class mass | \n\t\t\t\t\t\t\t1 10-5\n\t\t\t\t\t\t\t | \n\t\t\t\t\t\t||
0 – 150 kg | \n\t\t\t\t\t\t\tM1 class mass | \n\t\t\t\t\t\t\t1 10-4\n\t\t\t\t\t\t\t | \n\t\t\t\t\t\t||
0 – 1000 kg | \n\t\t\t\t\t\t\tM1-M2 mass | \n\t\t\t\t\t\t\t2 10-4\n\t\t\t\t\t\t\t | \n\t\t\t\t\t\t||
Temperature of glass thermometer | \n\t\t\t\t\t\t\t0 – 60 oC | \n\t\t\t\t\t\t\tWater bath | \n\t\t\t\t\t\t\t0,72 oC | \n\t\t\t\t\t\t\tMeasurement in laboratory by using comparison method | \n\t\t\t\t\t\t
60 – 150 oC | \n\t\t\t\t\t\t\tDry block oil bath | \n\t\t\t\t\t\t\t0,74 oC | \n\t\t\t\t\t\t||
Volume Piston pipettes | \n\t\t\t\t\t\t\t50 – 100 µl | \n\t\t\t\t\t\t\tin laboratory | \n\t\t\t\t\t\t\t0,100 µl | \n\t\t\t\t\t\t\tTS ISO 4787 TS EN ISO 8655-2 TS EN ISO 8655-6 | \n\t\t\t\t\t\t
200 µl | \n\t\t\t\t\t\t\t0,158 µl | \n\t\t\t\t\t\t|||
500 µl | \n\t\t\t\t\t\t\t0,315 µl | \n\t\t\t\t\t\t|||
1 ml | \n\t\t\t\t\t\t\t0,452 µl | \n\t\t\t\t\t\t|||
2 ml | \n\t\t\t\t\t\t\t1,209 µl | \n\t\t\t\t\t\t|||
5 ml | \n\t\t\t\t\t\t\t2,851 µl | \n\t\t\t\t\t\t|||
10 ml | \n\t\t\t\t\t\t\t5,991 µl | \n\t\t\t\t\t\t|||
Temperature meters with display | \n\t\t\t\t\t\t\t0 – 250 oC | \n\t\t\t\t\t\t\tIce bath and dry block oven | \n\t\t\t\t\t\t\t0,56 oC | \n\t\t\t\t\t\t\tMeasurement in laboratory by using comparison method | \n\t\t\t\t\t\t
250 – 600 oC | \n\t\t\t\t\t\t\t0,82 oC | \n\t\t\t\t\t\t|||
Moisture | \n\t\t\t\t\t\t\t20% - 70% RH | \n\t\t\t\t\t\t\tHumidity cabinet | \n\t\t\t\t\t\t\t1,4% RH | \n\t\t\t\t\t\t\tMeasurement in laboratory by using comparison method | \n\t\t\t\t\t\t
70% - 90% RH | \n\t\t\t\t\t\t\t2,2% RH | \n\t\t\t\t\t\t
The content of accreditation studies of calibration laboratories.
Calibration laboratories give services to all industry, textile, paint, food or health care etc. The company\'s working area is not important. The parameter to be measured is essential. For example, the mass for the weighing of food, rotational speed of the paint mixing device, hardness of the material used in manufacturing, the temperature of refrigerators used for drug store. The parameters are measured and a calibration certificate is prepared.
\n\t\t\t\tThe biomedical measurements in calibration laboratories are also performed generally as parameter measurements. The parameters can be classified as electrical parameters, pressure-vacuum parameters, temperature-humidity parameters, mass-volume parameters. An example study for accreditation of calibration laboratories can be seen in Table 1.
\n\t\t\t\t\n\t\t\t\tThe accreditation of calibration measurements is carried out via parameter measurements. Unlike other types of accreditation studies, parameter measurement is accredited for calibration laboratory. As of today, ISO IEC 17025 is taken as the basis for laboratory accreditation purposes. This standard is recognized worldwide. The requirements of this standard are provided for the general requirements on a laboratory\'s quality management system and technical competence. Laboratories accredited according to ISO IEC 17025 are re-evaluated periodically by the accreditation body and decision is made for the maintenance of accreditation based on results obtained.
\n\t\t\t\tLaboratories intending to maintain accreditation are required to participate inter-laboratory comparison and proficiency testing programs on their scope of accreditation and achieve successful results.
\n\t\t\t\t\n\t\t\tThe biomedical measurements in testing laboratories are performed on the basis of the medical device. The test procedures are prepared to test all parameters in the medical device. Defibrillators, ventilators...etc. are tested completely to measure all parameters in it. If there are many parameters in a device such as ECG parameters (electrical), blood pressure parameters (pressure), body temperature parameters (temperature), they are measured in according to the measurement procedures in the place of where medical device works and a certificate is prepared.
\n\t\t\t\tIn Turkey, the standard of 17025 is applied to testing laboratories for the medical devices. The content of the accreditation studies of testing laboratories can be seen in Table 2 and Table 3.
\n\t\t\t\t\n\t\t\t\t\t\t\t\t | \n\t\t\t\t\t\t\t\n\t\t\t\t\t\t\t\t | \n\t\t\t\t\t\t\t\n\t\t\t\t\t\t\t\t | \n\t\t\t\t\t\t
Electrical Safety Tests for all Electrical Biomedical Devices | \n\t\t\t\t\t\t\tEarth resistance | \n\t\t\t\t\t\t\tTS EN 60601-1 (item 8.7) | \n\t\t\t\t\t\t
Chassis leakage current | \n\t\t\t\t\t\t\tTS EN 60601-1 (item 8.7) | \n\t\t\t\t\t\t|
Patient leakage current | \n\t\t\t\t\t\t\tTS EN 60601-1 (item 8.7) | \n\t\t\t\t\t\t|
Patient auxiliary leakage current | \n\t\t\t\t\t\t\tTS EN 60601-1 (item 8.7) | \n\t\t\t\t\t\t|
Applied part leakage current | \n\t\t\t\t\t\t\tTS EN 60601-1 (item 8.7) | \n\t\t\t\t\t\t|
RMS chassis voltage | \n\t\t\t\t\t\t\tTS EN 60601-1 (item 8.9) | \n\t\t\t\t\t\t|
DC chassis voltage | \n\t\t\t\t\t\t\tTS EN 60601-1 (item 8.9) | \n\t\t\t\t\t\t|
Mains voltage | \n\t\t\t\t\t\t\tTS EN 60601-1 (item 8) | \n\t\t\t\t\t\t|
Device current | \n\t\t\t\t\t\t\tTS EN 60601-1 (item 8) | \n\t\t\t\t\t\t|
Performance-Safety Tests for Defibrillators | \n\t\t\t\t\t\t\tECG pulse test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 50.102.15) | \n\t\t\t\t\t\t
ECG amplitude test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 50.102.15) | \n\t\t\t\t\t\t|
ECG frequency test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 50.102.8) | \n\t\t\t\t\t\t|
ECG arythmia test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 56.8) | \n\t\t\t\t\t\t|
Energy test | \n\t\t\t\t\t\t\tTS EN 60601-2-4 (item 50) | \n\t\t\t\t\t\t|
Charge time test | \n\t\t\t\t\t\t\tTS EN 60601-2-4 (item 101) | \n\t\t\t\t\t\t|
Synchronized discharge test | \n\t\t\t\t\t\t\tTS EN 60601-2-4 (item 104) | \n\t\t\t\t\t\t|
Performance-Safety Tests for Electrosurgical Units | \n\t\t\t\t\t\t\tPower distribution test | \n\t\t\t\t\t\t\tTS EN 60601-2-2 (item 50.1) | \n\t\t\t\t\t\t
HF leak test | \n\t\t\t\t\t\t\tTS EN 60601-2-2 (item 19.3.101) | \n\t\t\t\t\t\t|
REM alarm test | \n\t\t\t\t\t\t\tTS EN 60601-2-2 (item 52) | \n\t\t\t\t\t\t|
Performance-Safety Tests for Pulse Oximeter (sPO2) | \n\t\t\t\t\t\t\tsPO2 performans test | \n\t\t\t\t\t\t\tTS EN ISO 9919 (item 50.101) | \n\t\t\t\t\t\t
ECG pulse test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 50.102.15) | \n\t\t\t\t\t\t|
sPO2 alarm test | \n\t\t\t\t\t\t\tTS EN ISO 9919 (item 104) | \n\t\t\t\t\t\t|
Performance-Safety Tests for Electrocardiography (ECG) | \n\t\t\t\t\t\t\tECG pulse test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 50.102.15) | \n\t\t\t\t\t\t
ECG amplitude test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 50.102.15) | \n\t\t\t\t\t\t|
ECG frequency test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 50.102.8) | \n\t\t\t\t\t\t|
ECG arythmia test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 56.8) | \n\t\t\t\t\t\t|
ECG ST test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 50.102.15) | \n\t\t\t\t\t\t|
ECG printer test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 50.102.16) | \n\t\t\t\t\t\t|
Performance-Safety Tests for Noninvasive Blood Pressure Monitor (NIBP) | \n\t\t\t\t\t\t\tNIBP performans test | \n\t\t\t\t\t\t\tTS EN 60601-2-30 (item 50.2) | \n\t\t\t\t\t\t
NIBP cuff pressure test | \n\t\t\t\t\t\t\tTS EN 60601-2-30 (item 22.4.1) | \n\t\t\t\t\t\t|
NIBP cuff leakage test | \n\t\t\t\t\t\t\tTS EN 60601-2-30 (item 50.2) | \n\t\t\t\t\t\t|
NIBP alarm test | \n\t\t\t\t\t\t\tTS EN 60601-2-30 (item 51.103) | \n\t\t\t\t\t\t|
Performance-Safety Tests for Aspirators | \n\t\t\t\t\t\t\tVacuum test | \n\t\t\t\t\t\t\tTS EN ISO 10079-1 | \n\t\t\t\t\t\t
Accuracy test | \n\t\t\t\t\t\t\tTS EN ISO 10079-1 | \n\t\t\t\t\t\t|
Flow test | \n\t\t\t\t\t\t\tTS EN ISO 10079-1 | \n\t\t\t\t\t\t
The content of accreditation studies of testing laboratories.
\n\t\t\t\t\t\t\t\t | \n\t\t\t\t\t\t\t\n\t\t\t\t\t\t\t\t | \n\t\t\t\t\t\t\t\n\t\t\t\t\t\t\t\t | \n\t\t\t\t\t\t
Performance-Safety Tests for Infusion Pumps | \n\t\t\t\t\t\t\tAir control test | \n\t\t\t\t\t\t\tTS EN 60601-1-24 (item 51-104) | \n\t\t\t\t\t\t
Flow accuracy test | \n\t\t\t\t\t\t\tTS EN 60601-1-24 (item 50-103) | \n\t\t\t\t\t\t|
Congestion performance test | \n\t\t\t\t\t\t\tTS EN 60601-1-24 (item 2-122) | \n\t\t\t\t\t\t|
Alarm test | \n\t\t\t\t\t\t\tTS EN 60601-1-24 (item 51-106) | \n\t\t\t\t\t\t|
Performance-Safety Tests for Aspirators | \n\t\t\t\t\t\t\tVacuum test | \n\t\t\t\t\t\t\tTS EN ISO 10079-1 | \n\t\t\t\t\t\t
Accuracy test | \n\t\t\t\t\t\t\tTS EN ISO 10079-1 | \n\t\t\t\t\t\t|
Flow test | \n\t\t\t\t\t\t\tTS EN ISO 10079-1 | \n\t\t\t\t\t\t|
Performance-Safety Tests for Shymphonometers | \n\t\t\t\t\t\t\tSystem leak test | \n\t\t\t\t\t\t\tTS EN 1060 | \n\t\t\t\t\t\t
Manometer test | \n\t\t\t\t\t\t\tTS EN 1060 | \n\t\t\t\t\t\t|
Accuracy test | \n\t\t\t\t\t\t\tTS EN 1060 | \n\t\t\t\t\t\t|
Performance-Safety Tests for Patient Monitor | \n\t\t\t\t\t\t\tECG pulse test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 50.102.15) | \n\t\t\t\t\t\t
ECG amplitude test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 50.102.15) | \n\t\t\t\t\t\t|
ECG frequency test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 50.102.8) | \n\t\t\t\t\t\t|
ECG arythmia test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 56.8) | \n\t\t\t\t\t\t|
ECG ST test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 50.102.15) | \n\t\t\t\t\t\t|
ECG printer test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 50.102.16) | \n\t\t\t\t\t\t|
Pacemaker test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 50.102.12) | \n\t\t\t\t\t\t|
ECG alarm test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 51.102) | \n\t\t\t\t\t\t|
Breath performance test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 50.102.8) | \n\t\t\t\t\t\t|
Breath alarm test | \n\t\t\t\t\t\t\tTS EN 60601-2-27 (item 51.102) | \n\t\t\t\t\t\t|
NIBP performans test | \n\t\t\t\t\t\t\tTS EN 60601-2-30 (item 50.2) | \n\t\t\t\t\t\t|
NIBP cuff pressure test | \n\t\t\t\t\t\t\tTS EN 60601-2-30 (item 22.4.1) | \n\t\t\t\t\t\t|
NIBP cuff leakage test | \n\t\t\t\t\t\t\tTS EN 60601-2-30 (item 50.2) | \n\t\t\t\t\t\t|
NIBP alarm test | \n\t\t\t\t\t\t\tTS EN 60601-2-30 (item 51.103) | \n\t\t\t\t\t\t|
IBP static pressure test | \n\t\t\t\t\t\t\tTS EN 60601-2-34 (item 51.102) | \n\t\t\t\t\t\t|
IBP dynamic pressure | \n\t\t\t\t\t\t\tTS EN 60601-2-34 (item 51.102) | \n\t\t\t\t\t\t|
IBP alarm test | \n\t\t\t\t\t\t\tTS EN 60601-2-34 (item 51.203.1) | \n\t\t\t\t\t\t|
sPO2 performans test | \n\t\t\t\t\t\t\tTS EN ISO 9919 (item 50.101) | \n\t\t\t\t\t\t|
sPO2 alarm test | \n\t\t\t\t\t\t\tTS EN ISO 9919 (item 104) | \n\t\t\t\t\t\t
The content of accreditation studies of testing laboratories (continued).
Inspection bodies which applied for accreditation must accomplish the requirements of standard ISO IEC 17020:2004. Inspection means investigation of the product design, product, service, process or the factory and their professional judgment based on the determination of the conformity of the general rules. Inspection bodies are conformity assessment companies. After the inspection, they transmit report to the customer, no certification. In Turkey, 17020 standard is applied for the radiography systems and clean room classification. The content of the accreditation studies of inspection bodies can be seen in Table 4.
\n\t\t\t\t\n\t\t\t\t\t\t\t\t | \n\t\t\t\t\t\t\t\n\t\t\t\t\t\t\t\t | \n\t\t\t\t\t\t\t\n\t\t\t\t\t\t\t\t | \n\t\t\t\t\t\t
kVp | \n\t\t\t\t\t\t\tIPEM Report No 32, European Commission Radiation Protection No 91 | \n\t\t\t\t\t\t|
Exposure time | \n\t\t\t\t\t\t\tIPEM Report No 32, European Commission Radiation Protection No 91 | \n\t\t\t\t\t\t|
Exposure repeatability and linearity | \n\t\t\t\t\t\t\tIPEM Report No 32, AAPM Report No 74, European Commission Radiation Protection No 91 | \n\t\t\t\t\t\t|
Tube output and stability | \n\t\t\t\t\t\t\tIPEM Report No 32, European Commission Radiation Protection No 91 | \n\t\t\t\t\t\t|
Filtration and half value layer | \n\t\t\t\t\t\t\tIPEM Report No 32, AAPM Report No 74, FDA 21 CFR 1020.30, European Commission Radiation Protection No 91 | \n\t\t\t\t\t\t|
Collimation | \n\t\t\t\t\t\t\tIPEM Report No 32, European Commission Radiation Protection No 91 | \n\t\t\t\t\t\t|
X-ray beam alignment | \n\t\t\t\t\t\t\tEuropean Commission Radiation Protection No 91 | \n\t\t\t\t\t\t|
Focal spot size | \n\t\t\t\t\t\t\tIPEM Report No 32, European Commission Radiation Protection No 91 | \n\t\t\t\t\t\t|
Automatic exposure control | \n\t\t\t\t\t\t\tIPEM Report No 32, European Commission Radiation Protection No 91 | \n\t\t\t\t\t\t|
Grid adjustment | \n\t\t\t\t\t\t\tEuropean Commission Radiation Protection No 91 AAPM Report No 74 | \n\t\t\t\t\t\t|
Leakage radiation | \n\t\t\t\t\t\t\tEuropean Commission Radiation Protection No 91 FDA 21 CFR 1020.30 | \n\t\t\t\t\t\t|
\n\t\t\t\t\t\t\t\t | \n\t\t\t\t\t\t\tkVp | \n\t\t\t\t\t\t\tEuropean Commission Radiation Protection No 91 IPEM Report No 91 | \n\t\t\t\t\t\t
Exposure time | \n\t\t\t\t\t\t\tEuropean Commission Radiation Protection No 91 IPEM Report No 91 | \n\t\t\t\t\t\t|
Tube output | \n\t\t\t\t\t\t\tEuropean Commission Radiation Protection No 91 | \n\t\t\t\t\t\t|
Patient entrance dose | \n\t\t\t\t\t\t\tIPEM Report N:91, European Commission Radiation Protection N 162 | \n\t\t\t\t\t\t|
Filtration and half value layer | \n\t\t\t\t\t\t\tEuropean Commission Radiation Protection No 91 FDA 21 CFR 1020.30 | \n\t\t\t\t\t\t|
X-ray beam size | \n\t\t\t\t\t\t\tEuropean Commission Radiation Protection No 91 IPEM Report No 91 | \n\t\t\t\t\t\t|
Patient focus distance | \n\t\t\t\t\t\t\tEuropean Commission Radiation Protection No 91 | \n\t\t\t\t\t\t|
Image repeatability | \n\t\t\t\t\t\t\tIPEM Report No 91 | \n\t\t\t\t\t\t|
Focus film distance | \n\t\t\t\t\t\t\tEuropean Commission European Guidelines for Quality in Breast Cancer Screening and Diagnosis | \n\t\t\t\t\t\t|
Tissue thickness sensor | \n\t\t\t\t\t\t\tIPEM Report 89 | \n\t\t\t\t\t\t|
Compression force | \n\t\t\t\t\t\t\tEuropean Commission Radiation Protection No 91, | \n\t\t\t\t\t\t|
kVp accuracy and repeatability | \n\t\t\t\t\t\t\tEuropean Commission European Guidelines for Quality in Breast Cancer Screening and Diagnosis, European Commission Radiation Protection No 91, ACR Mammography QC Manual | \n\t\t\t\t\t\t|
Tube output, tube output speed and repeatability | \n\t\t\t\t\t\t\tEuropean Commission European Guidelines for Quality in Breast Cancer Screening and Diagnosis, European Commission Radiation Protection No 91 IPSM Report N59, ACR Mammography QC Manual, IPEM Report No 89 | \n\t\t\t\t\t\t|
Tube output-mAs | \n\t\t\t\t\t\t\tIPEM Report No 91, IPEM Report No 89 | \n\t\t\t\t\t\t|
Filtration and half value layer | \n\t\t\t\t\t\t\tEuropean Commission European Guidelines for Quality in Breast Cancer Screening and Diagnosis, IPEM Report 89, ACR Mammography QC Manual | \n\t\t\t\t\t\t|
Mean glandular tissue dose | \n\t\t\t\t\t\t\tEuropean Commission European Guidelines for Quality in Breast Cancer Screening and Diagnosis, ACR Mammography QC Manual | \n\t\t\t\t\t\t|
Image contrast and high contrast resolution | \n\t\t\t\t\t\t\tEuropean Commission European Guidelines for Quality in Breast Cancer Screening and Diagnosis, European Commission Radiation Protection No 91 and 162, ACR Mammography QC Mn | \n\t\t\t\t\t\t|
Collimation, Grid factor and determination of grid errors | \n\t\t\t\t\t\t\tEuropean Commission European Guidelines for Quality in Breast Cancer Screening and Diagnosis, IPEM Report 89, European Commission Radiation Protection 91, ACR Mammo QC Manual | \n\t\t\t\t\t\t|
Image homogeneity and assessment of artifacts | \n\t\t\t\t\t\t\tEuropean Commission European Guidelines for Quality in Breast Cancer Screening and Diagnosis, IPEM Report 89, ACR Mammography QC Manual | \n\t\t\t\t\t\t|
Leakage radiation | \n\t\t\t\t\t\t\tEuropean Commission European Guidelines for Quality in Breast Cancer Screening and Diagnosis | \n\t\t\t\t\t\t|
\n\t\t\t\t\t\t\t\t | \n\t\t\t\t\t\t\tkVp | \n\t\t\t\t\t\t\tIPEM Report No 32, IPEM Report No 91, European Commission Radiation Protection No 91, AAPM Report No 74 | \n\t\t\t\t\t\t
Filtration and half value layer | \n\t\t\t\t\t\t\tIPEM Report No 32, IPEM Report No 91, IPEM Report No 32, European Commission Radiation Protection No 91, AAPM Report No 74 | \n\t\t\t\t\t\t|
Tube Output | \n\t\t\t\t\t\t\tIPEM Report No 32, AAPM Report N:70 | \n\t\t\t\t\t\t|
Maximum exposure speed | \n\t\t\t\t\t\t\tEuropean Commission Radiation Protection No 91 and 162, IPEM Report No 32, AAPM Report No 70 - 74 | \n\t\t\t\t\t\t|
Patient entrance dose | \n\t\t\t\t\t\t\tDraft European Commission Radiation Protection No 162, AAPM Report No 70, AAPM Report No 74 | \n\t\t\t\t\t\t|
Image amplified entrance dose | \n\t\t\t\t\t\t\tEuropean Commission Radiation Protection No 91 and 162, AAPM Report No 70 and 74 | \n\t\t\t\t\t\t|
Brightness control | \n\t\t\t\t\t\t\tIPEM Report N:32, AAPM Report No 70 | \n\t\t\t\t\t\t|
Gray scale | \n\t\t\t\t\t\t\tIPEM Report No 32 | \n\t\t\t\t\t\t|
Image artifacts | \n\t\t\t\t\t\t\tIPEM Report No 32 | \n\t\t\t\t\t\t|
Compliance of areas (exposured-displayed) | \n\t\t\t\t\t\t\tEuropean Commission Radiation Protection No 91, IPEM Report No 32 | \n\t\t\t\t\t\t|
High contrast and low contrast resolution | \n\t\t\t\t\t\t\tEuropean Commission Radiation Protection No 91, IPEM Report No 32 | \n\t\t\t\t\t\t|
Contrast detail | \n\t\t\t\t\t\t\tIPEM Report No 32 | \n\t\t\t\t\t\t|
\n\t\t\t\t\t\t\t\t | \n\t\t\t\t\t\t\tkVp | \n\t\t\t\t\t\t\tIPEM Report No 91 | \n\t\t\t\t\t\t
Exposure time | \n\t\t\t\t\t\t\tIPEM Report No 91 and 32, European Commission Radiation Protection No 91 | \n\t\t\t\t\t\t|
Exposure repeatability and linearity | \n\t\t\t\t\t\t\tIPEM Report No 91 and 32, European Commission Radiation Protection No 91, AAPM Report No 74 | \n\t\t\t\t\t\t|
Tube output and stability | \n\t\t\t\t\t\t\tIPEM Report No 91 and 32, European Commission Radiation Protection No 91 | \n\t\t\t\t\t\t|
Collimation | \n\t\t\t\t\t\t\tIPEM Report No 91 and 32, European Commission Radiation Protection No 91 | \n\t\t\t\t\t\t|
Gray scale | \n\t\t\t\t\t\t\tIPEM Report No 32 | \n\t\t\t\t\t\t|
High contrast and low contrast resolution | \n\t\t\t\t\t\t\tEuropean Commission Radiation Protection No 91, Draft European Commission Radiation Protection No 162, IPEM Report No 32 | \n\t\t\t\t\t\t|
Contrast detail | \n\t\t\t\t\t\t\tIPEM Report No 32 | \n\t\t\t\t\t\t|
kVp | \n\t\t\t\t\t\t\tIPEM Report No 32, | \n\t\t\t\t\t\t|
Half value layer test | \n\t\t\t\t\t\t\tIPEM Report No 32, | \n\t\t\t\t\t\t|
Position of external and internal scanning lights | \n\t\t\t\t\t\t\tIPEM Report No 32, IPEM Report No 91 | \n\t\t\t\t\t\t|
Coronal and Sagittal Alignment | \n\t\t\t\t\t\t\tIPEM Report No 32, IPEM Report No 91 | \n\t\t\t\t\t\t|
The slope of gantry | \n\t\t\t\t\t\t\tAAPM Report No 39 | \n\t\t\t\t\t\t|
Table axial motion accuracy | \n\t\t\t\t\t\t\tIPEM Report No 32, IPEM Report No 91, IEC 61223-2-6 | \n\t\t\t\t\t\t|
Table helical motion accuracy | \n\t\t\t\t\t\t\tIPEM Report No 32, IPEM Report No 91, IEC 61223-2-6 | \n\t\t\t\t\t\t|
Table distance sensor | \n\t\t\t\t\t\t\tIPEM Report No 32, IPEM Report No 91 | \n\t\t\t\t\t\t|
Computed tomography dose index (CTDI) | \n\t\t\t\t\t\t\tIPEM Report No 32, EC EUR 16262 | \n\t\t\t\t\t\t|
Tube output (CTDI Air) and linearity | \n\t\t\t\t\t\t\tIPEM Report No 32 | \n\t\t\t\t\t\t|
Slice thickness | \n\t\t\t\t\t\t\tIPEM Report No 32, IEC 61223-2-6 | \n\t\t\t\t\t\t|
CT number linearity | \n\t\t\t\t\t\t\tIPEM Report No 32, IPEM Report No 91 | \n\t\t\t\t\t\t|
Highcontrastresolution | \n\t\t\t\t\t\t\tIPEM Report N:32 and 91, IEC 61223-2-6 | \n\t\t\t\t\t\t|
Low contrast resolution | \n\t\t\t\t\t\t\tIPEM Report No 32 | \n\t\t\t\t\t\t|
Noise measurement | \n\t\t\t\t\t\t\tNCRPM Report No 99, IPEM Report No 32 and 91 | \n\t\t\t\t\t\t|
CT number uniformity | \n\t\t\t\t\t\t\tIPEM Report N:32 and 91, IEC 61223-2-6 | \n\t\t\t\t\t\t|
\n\t\t\t\t\t\t\t\t | \n\t\t\t\t\t\t\tImage homogeneity | \n\t\t\t\t\t\t\tAAPM Report of Task Group No 1 | \n\t\t\t\t\t\t
Image depth | \n\t\t\t\t\t\t\tAAPM Report of Task Group No 1 | \n\t\t\t\t\t\t|
Distance accuracy | \n\t\t\t\t\t\t\tAAPM Report of Task Group No 1 | \n\t\t\t\t\t\t|
Axial resolution | \n\t\t\t\t\t\t\tAAPM Report of Task Group No 1 | \n\t\t\t\t\t\t|
Lateral resolution | \n\t\t\t\t\t\t\tAAPM Report of Task Group No 1 | \n\t\t\t\t\t\t|
Dead zone | \n\t\t\t\t\t\t\tAAPM Report of Task Group No 1 | \n\t\t\t\t\t\t|
Cyst diameter | \n\t\t\t\t\t\t\tAAPM Report of Task Group No 1 | \n\t\t\t\t\t\t|
\n\t\t\t\t\t\t\t\t | \n\t\t\t\t\t\t\tNegatoskop brigthness and levels of bright of viewing room | \n\t\t\t\t\t\t\tIPEM Report 89, IPEM Report No 32, European Commission European Guidelines for Quality in Breast Cancer Screening and Diagnosis, ACR Mammography QC Manual | \n\t\t\t\t\t\t
The content of accreditation studies of inspection bodies.
In Turkey, accreditation studies about biomedical calibration are performed in 3 different types. Calibration laboratories, testing laboratories and inspection bodies. Normally, although the scope of their applications seems like they are nested, they are separated from each other with little detail. Inspections of radiography devices and clean rooms are performed by inspection bodies. Other medical devices except for pipettes, thermometers, humidity meters that must be measured in laboratory conditions, are tested by testing laboratories and they are accredited in according to the standard of ISO IEC 17025. In calibration laboratories, it is essential to ensure appropriate environmental conditions for measurements. Because of this, measurements that require special measuring environment are performed in calibration laboratories.
\n\t\t\tIf the differences and details of accreditation studies about biomedical calibration measurements are known by the health organizations, to make the right choice in the selection of calibration laboratory, testing laboratory or inspection body is inevitable.
\n\t\tQuality service can be only taken from the accredited laboratories. As a matter of fact, the national and international procedures of accreditation say, “There is not an obligation. The accreditation depends on the base of voluntary.” (TURKAK website).
\n\t\t\tEven if accreditation is not obligated, the expectation in medical calibration measurements is that the personnel must be professional, the calibration procedures and the test devices, calibrators must be appropriate to the international standards.
\n\t\tI would like to thank the co-operation of the calibration laboratories, the testing laboratories and the inspection bodies that present the content of their accreditation studies.
\n\t\tTypical commercial and civilian satellite systems take about 2–3years to build and launch [1, 2, 3, 4], while military systems take between 7 and 10 years [5, 6]. A typical production flow for assembling and launching of a space vehicle is presented in Ref. [6] and redrawn in Figure 1 as introduction steps for better understanding of the design, build and launch of a satellite system. This chapter focuses on practical design issues for satellite Bus’ and mission PL’s system/subsystem components builds, and corresponding interface-design’s challenges associated with satellite Bus integration, mission PL integration, and satellite system integration. A survey of existing commercial, civilian and military satellite systems revealed that a typical satellite Bus includes the following modular components [7, 8, 9, 10, 11, 12, 13, 14, 15, 16]:
Bus Subsystem 1—Bus TX/RX Antenna Subsystem (BAS): Provide Bus’s Receive (RX)/Transmit (TX) antennas and associated Bus’s antenna beam control functions;
Bus Subsystem 2—Bus Communication RF Front-End-Back-End Subsystem (BCom-RFS): Provide Low Noise Amplifier (LNA), High Power Amplifier (HPA), satellite Bus Down/Up Radio Frequency (RF)-to-Intermediate Frequency (IF) conversion, and Analog-to-Digital/Digital-to-Analog conversion functions—Note that typical HPAs are Traveling Wave Tube Amplifier (TWTA) and Solid State Power Amplifier (SSPA), and some advanced satellite transponders use Linearized TWTA (L-TWTA) or L-SSPA in the RF Back-End Subsystem;
Bus Subsystem 3—Bus Command & Data Handling Subsystem (BC&DHS): On-board computer that interfaces with all Bus components;
Bus Subsystem 4—Bus Telemetry-Tracking & Command Subsystem (BTT&CS): Process uplink satellite Bus command data, perform satellite tracking functions and provide downlink Bus telemetry reporting satellite Bus’s heath and conditions;
Bus Subsystem 5—Bus Electrical Power Subsystem (BEPS): Provide and regulate Bus power;
Bus Subsystem 6—Bus Thermal Control Subsystem (BTCS): Maintain Bus’ thermal environments;
Bus Subsystem 7—Bus Altitude and Determination Control Subsystem (BADCS): Provide satellite stabilization, control and positioning;
Bus Subsystem 8—Bus Propulsion Subsystem (BPS): Provide propulsion functions for satellite maneuvering;
Bus Subsystem 9—Bus Communication Security Subsystem (BCOMSEC): Provide Bus data encryption and decryption functions to protect data from intruders. Typically, BCOMSEC is tightly coupled with BTT&CS;
Bus Subsystem 10—Bus Structure & Mechanism Subsystem (BS&MS): Provide structure and mechanism to mount all satellite Bus components.
A typical satellite system production flow (redrawn from [
Similarly, our survey also revealed that a typical mission PL consists of the following modular components [7, 8, 9, 10, 11, 12, 13, 14, 15, 16]:
PL Subsystem 1—PL PAS: Similar to BPAS but for mission PL;
PL Subsystem 2—PL Com-RFS: Similar to BCom-RFS but for mission PL;
PL Subsystem 3—PL Digital Processing Subsystem (PDPS): Provide mission specific processing functions. For SATCOM missions, specific processing functions can be dynamic resources control, channelization processing, etc. For PNT missions, the functions can be time transfer processing functions. For imaging/sensing missions, the functions can be image preprocessing functions;
PL Subsystem 4—PL C&DHS: Similar to BC&DHS but for mission PL;
PL Subsystem 5—PL TT&CS: Similar to BTT&CS but for mission PL;
PL Subsystem 6—PL EPS: Existing PLs use power supply from satellite BEPS;
PL Subsystem 7—PL TCS: Maintain PL’s thermal environments;
PL Subsystem 8—PL ADCS: Existing PLs use ADCS from the satellite BADCS;
PL Subsystem 9—PL PS:: Existing mission PLs use PS from the satellite BPS;
PL Subsystem 10—PL COMSEC: Similar to BCOMSEC but for mission PL;
PL Subsystem 11—PL Frequency & Timing Subsystem (PFTS): Provide reference frequency and timing functions to meet specific mission requirements;
PL Subsystem 12—PL Transmission Security Subsystem (TRANSEC): Provide security functions to combat unintentional and/or intentional Radio Frequency Interference (RFI) (e.g., frequency hopping/de-hopping, frequency spreading/de-spreading);
PL Subsystem 13—PL Specific Mission Suite (SMS): Provide specific mission PL processing functions depending on whether the mission is Satellite Communications (SATCOM) mission or Position Navigation and Timing (PNT) mission or Imaging/Sensing mission [7, 8, 9, 10, 11, 12, 13, 14, 15, 16];
PL Subsystem 14—PL Structure & Mechanism Subsystem (BS&MS): Provide structure and mechanism to mount all mission PL components.
In practice, the above satellite Bus modular components can be found in the following typical satellite Busses [7, 11, 14]:
Loral Satellite Bus 1300 or Loral 1300
Lockheed Martin (LM) A2100A/AX-Land Mobile/AX-High Power
Boeing 702HP/HP-GEM/MP/702SP and 502.
For achieving optimum weight and power, existing satellite Bus and mission PL are tightly coupled together with customized interface design. The industry trends for the design and build of future satellite systems are moving toward OSA using MOSA principles, in which the satellite Bus is loosely coupled with the mission PL using “Open” and widely accepted interface standards. The key communication linkage between a satellite Bus and a mission PL is the communication data Bus. Currently, majority of satellite Busses employ the standard 1553 data Bus for data communications among Bus components, and between the satellite Bus and mission PL components. The communications over 1553 data Bus is limited to 1 Mega bit per second (Mbps). Recently, there was an advanced development effort that was funded by the U.S DOD to develop new 1553 standards called 1553 Enhanced Bit Rate (EBR–1553) increasing the speed to 10 MB/s [17]. The EBR-1553 requires a star/hub topology to provide the higher data rate and additional components to implement the architecture. For data rates larger than 10 Mbps, space industry trend is moving toward SpaceWire data Bus that was recently developed in Europe for use in commercial satellites and scientific spacecraft [18].
The objective of this chapter is three-fold: (1) Provides an overview of existing modular satellite Bus, mission PL architectures and related communication data Busses, (2) Discusses future trends on the modular and open design and build of satellite Bus and mission payload using MOSA principles, and (3) Addresses the practical design challenges associated with “Modular” and “Open” design for future satellite Bus and mission PL. The chapter is organized as follow: (i) Section 2 describes existing modular satellite Bus and mission PL architectures and related communication data Busses; (ii) Section 3 presents industry view on “Open” and “Close” interfaces for connecting satellite system components and existing popular standards; (iii) Section 4 discusses the interface design challenges and provides an overview of MOSA and related DOD Guidance and assessment tools for MOSA implementation; (iv) Section 5 provides examples how to transition modular satellite Bus and mission PL architectures to modular-and-open architectures using MOSA implementation approach and tools in Section 4; and (v) Section 6 concludes the chapter with remarks on the benefits associated with the proposed approach.
Figure 2 describes an overview of existing satellite systems, consisting of a satellite Bus, a mission PL and a typical set of interfaces between the Bus and PL using a standard data Bus. A typical set of interfaces between the satellite Bus and a mission PL includes seven interface types, namely: (i) Physical & Mechanical Interface, (ii) Electrical/Power/Cable Interface, (iii) Grounding Interface, (iv) Software & Data Interface, (v) Electromagnetic Compatibility (EMC)/ Electromagnetic Interference (EMI)/Electromagnetic Pulse (EMP) and Electro Static Discharge (ESD) Interface, (vi) Thermal Interface, and (vii) Frequency & Timing (F&T) Interface. This section focuses on satellite Bus and mission PL architectures and the data interfaces between them. Subsections 2.1 and 2.2 describe existing satellite Bus and mission PL architectures along with related interfaces and industry standards, respectively. Subsection 2.3 discusses existing standard 1553 data Bus and the pushes from space industry moving toward military standard 1553-B data Bus (MIL-STD-1553-B) and high-data-rate SpaceWire data Bus.
Overview of existing satellite Systems using standard 1553 data bus.
As described in Section 1, existing satellite Bus architecture includes typical 10 modular components, namely, BAS, BComRFS, BC&DHS, BTT&CS, BEPS, BTCS, BADCS, BPS, BCOMSEC and BS&MS. A functional description for each of these modular Bus components is also described in Section 1. Figure 3 illustrates a notional block diagram for existing modular satellite Bus architecture. The figure shows that space industry has used the modular design concept to architect the satellite Bus, where common functions are group together and then isolate or separate from the other group of functions. As an example, BAS consists of a group of antenna components and control functions (e.g., antenna pointing, beamforming, etc.), which is separated and isolated from BComRFS. It is important to note that the figure also shows how these satellite Bus components are connected together, i.e., the lines with arrows connecting them. These lines represent the interfaces among the Bus components, where the interface can be any of the seven interface types described above. Below is a list of some of the existing interfaces and associated standards for existing satellite Bus based on National Aeronautical and Space Administration (NASA), European Space Agency (ESA), U.S. DOD and international Consultative Committee for Space Data System (CCSDS) standards [19, 20, 21, 22, 23, 24, 25, 26]:
Typical NASA Electrical/Power/Cable Interface Standards [19, 20]:
Satellite Bus shall protect its own electrical power system via overcurrent protection devices on its side of the interface.
Satellite Bus shall deliver a maximum transient current on any Power Feed Bus of 100% (that is, two times the steady state current) of the maximum steady-state current for no longer than 50 ms.
Bus Survival Heaters, which are elements of the Bus thermal subsystem, shall be required to have power to heat certain satellite Bus components during off-nominal scenarios when the BEPS power is not fully energized.
Typical U.S. DOD EMC/EMI/EMP/ESD Interface Standards [21]:
Power line conducted emissions for satellite Bus equipment shall meet the EMC interface specification specified in SMC Standard Handbook, SMC-S-008, Section 6, 6.01, 6.02, 6,03, 6.04, 6.05, 6.06, 6.07, and 6.08.
Power line conducted susceptibility for satellite Bus equipment shall meet the EMC interface specification specified in SMC Standard Handbook, SMC-S-008, Sections 6, 6.10, 6.11, 6.12, 6.13, 6.14, 6.15, 6.16, 6.17, 6.18 and 6.19.
ESD susceptibility for satellite Bus equipment shall meet the EMC interface specification specified in SMC Standard Handbook, SMC-S-008, Section 6, 6.43.
EMP susceptibility for satellite Bus equipment shall meet the EMC interface specification specified in SMC Standard Handbook, SMC-S-008, Section 6, 6.45.
Typical NASA Grounding Interface Standards [20, 22]:
Satellite Bus EPS should ground in a way that reduces introducing stray currents or ground loop currents into the satellite Bus components.
Satellite Bus ground interface shall follow NASA single-point ground or multiple-point ground architecture.
Typical NASA Thermal Interface Standards [19, 20]:
A conductive heat transfer of 15 W/m2 or 4 W shall be considered small enough to meet the intent of being thermally isolated.
Typical Software & Data Interface Standards [19, 20, 23, 24, 25, 26]:
Satellite Bus command and telemetry data formats shall be NASA Unified S-Band (USB)/CCSDS standards or U.S. DOD Space-Ground Link Subsystem (SGLS) standards. Note that (i) most of NASA and ESA standards are CCSDS compliance for interoperability purpose, and (ii) some military systems have both USB and SGLS capabilities.
Satellite Bus “Safe Mode” is a combined satellite Bus components hardware and software configuration that shall be designed to protect the components from possible internal or external harm while making minimal use of satellite Bus resources (e.g., power).
Satellite Command SAFE Mode shall be required to protect and preserve satellite Bus components under anomalous and resource constrained conditions.
Satellite Bus components shall respond to uplink commands from the Satellite Operation Center (SOC) to suspend and resume the transmission of the Components’ telemetry data. For commercial satellite systems, SOC can also control the mission PL.
Existing notional modular satellite bus architecture.
For military applications, majority of satellite Busses are usually designed using contractor’s custom designed interfaces and very tightly couple together to reduce weight, size and power. It is for this reason, current military satellite BTT&CS component also include the COMSEC component. For commercial applications, satellite developers are also concerned with weight, size and power reduction, but they are also concerned with component refresh and upgrade without redesigning the satellite Bus, hence commercial satellites tend to use modular Bus components and widely accepted interface standards to connect the internal Bus components. Industry views on the “open” and “close” interfaces will be addressed in Section 4.
As pointed out in Section 1, existing mission PL architecture consists of 14 modular components, but there are three PL components that rely on the satellite Bus’ design, namely, PL EPS, PL ADCS and PL PS. Therefore, the mission PL architecture usually has 11 modular components, including PL AS, PL Com-RFS, PDPS, PL C&DHS, PL TT&CS, PL TCS, PL COMSEC, PFTS, PL TRANSEC, PL SMS and PL S&MS. A functional description for each of these mission PL modular components is also provided in Section 1. Figure 4 presents a notional block diagram for existing modular mission PL architecture. Similar to the satellite Bus design, the space industry has also applied the modular design concept to architect the mission PL. Below is a list of some of the existing interfaces and associated standards for existing mission PL leveraged from NASA, ESA, U.S. DOD and international CCSDS standards [19, 20, 21, 22, 23, 24, 25, 26]:
Typical NASA Electrical/Power/Cable Interface Standards [19, 20]:
Sizing all components of the mission PL power harness, such as the wires, connectors, sockets, and pins to the peak power level shall be required by the mission PL equipment in addition to satellite Bus to prevent damage to the power harnessing.
PL Survival Heaters shall be required to have power to heat certain mission PL components during off-nominal scenarios when the BEPS power is not fully energized.
Typical U.S. DOD EMC/EMI/EMP/ESD Interface Standards [21]: Similar to satellite Bus discussed above but for mission PL.
Typical NASA Grounding Interface Standards [20, 22]: Similar to satellite Bus discussed above but for mission PL.
Typical NASA Thermal Interface Standards [19, 20]:
The mission PL thermal design should be decoupled from the satellite Bus at the mechanical interface between the satellite Bus and neighboring mission payload to the maximum practical extent.
A conductive heat transfer of 15 W/m2 or 4 W shall be considered small enough to meet the intent of being thermally isolated.
Typical Software & Data Interface Standards [19, 20, 23, 24, 25, 26]:
Mission PL command and telemetry data formats shall be NASA USB/CCSDS standards commercial applications or U.S. DOD SGLS standards for military applications. Some military systems have both USB and SGLS capabilities.
PL “Safe Mode” is a combined mission PL components hardware and software configuration that shall be designed to protect the PL components from possible internal or external harm while making minimal use of satellite Bus resources (e.g., power).
PL Command SAFE Mode shall be required to protect and preserve mission PL components under anomalous and resource constrained conditions.
Mission PL components shall respond to uplink commands from Mission Control Center (MCC) to suspend and resume the transmission of the mission PL components.
Mission PL shall be responsible for on-board mission data storage capabilities.
Existing notional modular Mission payload architecture.
For most commercial applications, the MCC can be merged with the SOC, and the mission PL TT&CS (PTT&CS) and PL CD&HS (PCD&HS) components can be incorporated into satellite (i) Bus TT&C (BTT&CS) and (ii) Bus CD&HS (BCD&HS) components, respectively. Similar to the satellite Bus interfaces design, for military applications, the mission PL components are tightly coupled using contractor’s custom designed interfaces. For commercial applications, the mission PL components are loosely coupled using widely accepted open interfaces.
Subsections 2.3.1 and 2.3.2 provide an overview of standard 1553 and SpaceWire communication data Busses, respectively.
Existing commercial, civilian and military satellite data Busses have been using Military Standard 1553B (MIL-STD-1553B) data Bus for communications among satellite Bus and mission PL components. Figure 5 describes a typical MIL-STD-1553B System [17, 27, 28]. This figure uses MIL-STD-1553B terminologies: (i) the Bus Controller (BC) is considered as an Intelligent Terminal (IT) that is located in the satellite mission computer, which is usually referred to as a Satellite Bus C&DH component, and (ii) Remote Terminal (RT) is considered as a slave terminal that is located in satellite platform components, which can be located in any satellite Bus or mission PL components.
Typical civilian and commercial MIL-STD-1553B satellite Systems.
Figure 5 shows a typical commercial satellite system with RTs located in both satellite Bus and mission PL components. As an Example, the RTs located in satellite components are BAS, BADCS, BTCS and BTT&CS; and RTs located in the mission PL components are PAS, PTCS, PDPS, PTRANSEC, and PFTS. For military applications, the Mission Computer (MC) can be located in both satellite Bus and mission PL, where the MC in the satellite Bus is responsible for all control functions associated with the satellite operations and MC in the mission PL is responsible for all control functions related to the mission PL operations.
SpaceWire (SpW) is an industry standard with protocol derived from IEEE-1355 and ECSS-E50-12C managing by the international SpW working Group [18, 29, 30]. The SpW standard is a self-managing serial protocol that provides a high-speed data rates from 2 to 400 Mbps, and low power serial interface using LVDS1 Drivers with distances up to 30 feet while offering a flexible simple user interface. Figure 6 illustrates typical uses of SpW data Bus with a PCD&HS, a SpW Router and SpW cables for connecting mission PL components. Some examples of existing satellite programs employed SpaceWire standard are: TacSat (part of the U.S. Operationally Responsive Space Program), NASA Lunar Reconnaissance Orbiter (Orbiting the Moon taking high resolution images), ESA Sentinel-3 (a pair of satellites providing operational Earth observation services using optical and microwave instruments), and Japanese NEC NEXTTAR (one of the first spacecraft designed using SpW for all of its onboard communications).
Typical civilian and commercial SpaceWire satellite Systems.
Figure 7 presents the space industry view on open and close interface design. This view separates the interface design into two categories, namely, Contractor Proprietary Interface and Contractor Non-Proprietary Interface. Under this view, the interface standards are then classified into two categories, namely, Preferred and Non-Preferred Interface Standards. Based on this view, Section 3.1 defines open interface design, and Section 3.2 defines close interface design. Section 3.3 provides a list of existing popular open standards widely accepted by space industry.
Industry view on open and closed interfaces design.
From Figure 7, the open interface design falls into the contractor non-proprietary design category. For the interface design to be open, the interface design shall not be contractor proprietary and that the interface shall use either popular open interface standards widely accepted by space industry or open interface standards with little market support and narrowly used by space industry. Thus, a popular open interface design is a non-proprietary design that uses popular open interface standard that is widely used by space industry. The benefits of open interface design for the satellite buyers are (i) improving competition allowing various space vendors (or contractor) to build open satellite Bus and mission PL subsystem components, (ii) ease of refresh and technology upgrade allowing to swap subsystem components without impacting the overall system, (iii) ease of adapting to new requirements and operational threats, (iv) incorporating innovation by allowing operational flexibility to configure and reconfigure a mission PL quickly to meet rapidly changing operational requirements, (v) enabling cost saving and cost avoidance during the design and sustainment phases by reusing technology and Software/Hardware/Middleware (SW/HW/MW) components, and using existing standardized HW/SW/MW parts and modules, and (vi) improving interoperability where severable HW/SW/MW modules can be changed independently.
As shown in Figure 7, the close interface design shall fall into contractor proprietary category. For an interface design to be close, it shall be contractor proprietary and that the interface shall use either close interface standards with little market support narrowly used by space industry or popular closed interface standards widely used by space industry. Thus, a popular close interface design is a contractor proprietary design that uses popular closed interface that is widely used by space industry. The key benefits of close interface design are the potential reduction of weight, size, power and manufacturing cost.
Based on Figure 7, the criteria for popular open standards are (i) publicly available and widely used by both satellite Bus and mission PL vendors, (ii) community and/or industry consensus-based that are matured and stable, and (iii) technically adequate for all future commercial, civilian and military satellite systems. Following is a list of current popular standard organizations and widely adopted open standards [18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31]:
Consultative Committee for Space Data Systems (CCSDS) Standards: is a multi-national forum for the development of communications and data systems standards for spaceflight. The goal is to enhance governmental and commercial interoperability and cross-support, while also reducing risk, development time and project costs.
AIAA Space Plug-and-play Avionics (SPA) Standard: SPA is a set of AIAA standards developed for spacecraft platform, subsystem, and component (including payload) developers for integrating plug-and-play characteristics into spacecraft structures, avionics, and hardware and software components to promote their rapid integration. The SPA community anticipates adding protocols (e.g., Ethernet as SPA-E) as the PnP capabilities are normalized.
MIL-STD-1553 Standard: is a military standard published by the United States Department of Defense that defines the mechanical, electrical, and functional characteristics of a serial data Bus.
SpaceWire Standard: is a spacecraft communication network standard based in part on the IEEE 1355 standard of communications. It is coordinated by the European Space Agency (ESA) in collaboration with international space agencies including NASA, Japanese Space Agency (JAXA) and Russian Federal Space Agency (RKA).
NASA/SMC/Aerospace Hosted Payload Interface Design (HPID): this design guideline provides a prospective Instrument Developer with technical recommendations to assist them in designing an Instrument or Payload that may be flown as a hosted payload on commercial satellites flown in Low Earth Orbit (LEO), or Geostationary Earth Orbit (GEO).
SQL for databases specified in ANSI ISO/IEC 9075–1, ISO/IEC 9075–2, ISO/IEC 9075–3, ISO/IEC 9075–4, ISO/IEC 9075–5.
HTML for presentation layer specified in XML 1.0 www.webstandards.org.
XML for data transfer.
Web Services for remote system calls.
U.S. Space and Missile Systems Center (SMC) approved a project for developing Common Payload Interface Specification (CoPaIS) standard for satellite-to-payload Command and Data Handling (C&DH) interface intended for all future SMC procured medium to large satellites [31].
Other popular standards: MIL-STD-1553B, CAN Bus, RS-422 (TTC-B01 Protocol)/EIA/TIA-422, RS-422 (PC-Protocol).
This section addresses the design challenges and is divided into four subsections, including: (i) Subsection 4.1 discusses interface design and practical design issues; (ii) Subsection 4.2 introduces MOSA concept; (iii) Subsection 4.3 presents DOD MOSA guidance and the U.S. Naval Open Architecture (NOA); and (iv) Subsection 4.4 discusses MOSA tools and approach for MOSA implementation that addresses the design issues identified in Subsection 4.1.
The interfaces between satellite subsystem components can be SW, HW or MW interfaces. The design and build of these interfaces are well incorporated into any satellite subsystem components “Design Product” and associated “Design Process”.
The Design Product includes System Architecture, Interface Product, Independent Verification and Validation (IV&V) Test Plan, Schedule, Design Approach, Acceptance Criteria, and System-Built Product.
For MOSA, the Design Process is expected to incorporate MOSA into: Architecture Process, Interface Management, IV&V Process, and System Engineering and Integration (SE&I) Process. The Interface Product and its open interface design using MOSA along with the Interface Management are the key challenges in the development of open-and-modular satellite systems. The key design challenges for the design and build of open-and-modular satellite systems are:
Challenge 1: Determination of Key Open Subsystem (KOSS): This is also known as KOSS Selection. Ideally, all modular subsystem components should be made open. But this is not practical, because some interfaces need to be customized using close interface design due to weight, size and power reduction requirements. The key challenge here is to identify a set of criteria that can be used for KOSS selection. Subsections 4.3 and 4.4 will address this challenge.
Challenge 2: Designation of Key Interfaces for the Selected KOSS: Satellite system designers need to identify a subset of selected set of KOSS components that can be designated as key interfaces. The key challenge here is to identify a business case for the designated key interfaces. Subsections 4.3 and 4.4 will describe selection criteria and tool to address this challenge.
Challenge 3: Selection of Open Standards for the Designated Key Interfaces: Selection of the popular and open standards for the designated key interfaces is also a potential challenge for the designers. The selection should be based on the cost, required technical specification and availability of “open” products in the market and their usage by space industry. SubSection 3.3 above provides a list of some existing open and popular standards. Subsection 4.4 will discuss how to resolve this challenge by developing a business case to justify the selection of key interfaces and associated open standards.
Challenge 4: Management of Key Open Interfaces: Not all identified key interfaces in Challenge 2 can be designated an open interface standard at the initial system design phase due to market unavailability. Hence, managing these interfaces can be a potential challenge ensuring that they will be “open” by the time of Full Operational Capability (FOC) deployment. Section 4.3 discusses DOD guidance for managing key interfaces for military satellite system development.
U.S. DOD recommends OSA design using MOSA principles for future military satellite system development with a goal to achieve a balance between business and technical objectives that make a business sense in terms of (i) increase competition and lower system acquisition cost, and (ii) lower sustainment cost over its life cycle. MOSA design approach requires to implement five MOSA principles, including two Business (B) and three Technical (T) principles [1, 2]. Figure 8 captures these five B and T principles. Recently, U.S. Navy augmented MOSA principles with addition five Naval Open Architecture (NOA) principles, including two business and three technical principles as shown in Figure 8 [3].
MOSA and U.S. NOA approach.
Subsections 2.1 and 2.2 provide current implementation of the Technical principle 1 (T1) for the modular design of satellite Bus and mission PL, respectively. The remaining Subsections 4.3 and 4.4 discuss the implementation of T2, T6, Business principle 3 (B3), and B4 using DOD guidance for addressing the challenges presented in Subsection 4.1.
MOSA mandated the space system technical requirements be based on the maximum extent practicable on open standards as indicated in Section 3.2 of the U.S. DOD Guidebook for Program Managers [1]. The book provides MOSA2 guidelines and contract language for generating a Request for Proposal (RFP) [1]. At the minimum, the RFP shall incorporate the following MOSA tasks that can help to minimize the MOSA implementation risk in the design, build and test of new satellite systems:
Design the open system architecture using open interfaces. Implement the open interfaces using open standards for connecting HW-to-HW, and SW-to-SW.
The satellite system design shall accommodate growth and provide open interface standards to allow future reconfiguration and addition of new capabilities without large-scale redesign of the system.
Develop a capability roadmap for the system covering the life of the system following the completion of the rapid prototyping contract phase.
Address “Commercial Off the Shelf/Non-Developmental Item and Open System Software Licenses,” including Open Source Software, Verification of Open Architecture, Modular Open Systems Approach Metrics to be Reported, Modular Open System Approach Analysis Report.
Generate Open System Management Plan (OSMP) to capture all MOSA activities, technology roadmaps; Define and track MOSA metrics; Update roadmap. Following is a list of MOSA metrics that should be used to demonstrate an open satellite system:
Number and location of private extensions on open interfaces;
Contractor use of company private extensions on open standard middleware;
Open Software Design Tool Kits/Component Design Tool Kits (OSDTK/CDTK) will be provided with a minimum of Government Purpose Right (GPR); Minimal license fees may apply for COTS items;
Percentage of Chief Engineers, IPT Leads and program team members on architecture, software, logistics and Test & Evaluation trained in Open Systems Architecture and the MOSA tools;
Future Competition Strategy included in the OA Business plan within the OSMP;
MOSA (or OSA) requirements flowed down to sub-tier suppliers and recorded in IBM Rational® DOORS® requirements database or an MBSE digital model.
Design a system that consists of hierarchical collections of software, hardware, and firmware Configuration Items (CI’s). Document in the MOSA Analysis Report its modularization choices for the system design and any tradeoffs performed in accordance with the OA verification plan.
Document any processes or applications necessary to support MOSA in the MOSA Analysis Report.
The above U.S. DOD’s guidance encourages the satellite system designers to consider the above MOSA items in the design and build of the modular and open satellite Bus and mission payload for future space systems. The following section presents a proposal for assisting the satellite system designers to implement these MOSA items along with assessment tools provided by U.S. DOD.
It is observed that the U.S. DOD, U.S. civilian agencies (e.g., NASA, NOAA, etc) and U.S. satellite manufacturers/suppliers (e.g., LM, Boeing, Northrop Grumman (NG), Raytheon, L3, etc) are investigating approaches for the modular and open design and build of satellite Busses and mission PL’s using MOSA modular and open design principles. Figure 9 proposes an approach to design and build of future modular and open satellite Busses and mission PLs, and allowing the satellite buyers to: (i) Buy the satellite Bus (see Path A of the figure) and mission PL (see Path B) from different satellite manufacturers/suppliers, (ii) Have an option to choose a third satellite vendor to integrate the satellite Bus and mission PL (see Path C).
Proposed implementation approach for design and build of satellite Systems allowing buyers to acquire satellite bus and Mission PL independently.
The proposed MOSA implementation approach shown in Figure 4 consists of six basic steps that are incorporated into three execution paths, namely, Path A, Path B and Path C:
Path A is for the satellite Bus manufacturer/supplier. This path has three basic steps:
Step I-A: Develop Modular satellite Bus Architecture (MoBA). The MoBA subsystem components are described in Sections 1 and 2 (see Figure 3).
Step II-A: Designate KOSS’s and select open standards for all internal satellite Bus subsystem components. Open interface standards selection and designation of KOSS are discussed in Sections 3 and 4.
Step III-A: Design and build Open Modular satellite Bus System (OMoBS). This step is achieved by identifying all potential KOSS’s from the satellite Bus to any mission PL’s, i.e., the selected KOSS’s should be independent of mission types. The satellite Bus manufacturer is responsible for integrating all Bus components and have the satellite Bus ready for sale.
Path B is for the mission PL manufacturer/supplier. This path also has three basic steps that are similar to Path A:
Step I-B: Develop Modular Mission PL Architecture (MoPA). The MoPA subsystem components are also described in Sections 1 and 2 (see Figure 4).
Step II-B: Designate KOSS’s and select open standards for all internal Mission PL subsystem components. Open interface standards selection and designation of KOSS for mission PL are also discussed in Sections 3 and 4.
Step III-B: Design and build Open Modular Mission PL System (OMoPS). This step is achieved by identifying all potential KOSS’s from the any mission PL’s to satellite Bus, i.e., the selected KOSS’s should be independent of mission types. The mission PL manufacturer is responsible for integrating all mission PL components and have the PL ready for sale.
Path C is for the satellite system integrator. This path has additional three new steps:
Step IV: The system integrator works with satellite Bus and mission PL manufacturers to develop a satellite system interface specification specifying all “open” and “close” interfaces between the mission PL-and-satellite Bus. All open interfaces between the mission PL-and-satellite Bus shall be selected to meet the business and performance objectives approved by the buyer. The system integrator performs satellite Bus and mission PL integration using the approved interface specification.
Step V: System integrator performs system test and verification subject to buyer’s approval.
Step VI: System integrator delivers the satellite system to the buyer.
DOD has also developed MOSA tools to assist MOSA implementation and assessment of military satellite Bus and mission PL “Openness”. These tools can also be used for civilian and commercial applications. The DOD tools include MOSA Program Assessment and Rating Tool (PART), Open Architecture Assessment Tool (OAAT), and Key Open SubSystem (KOSS) Tool:
MOSA PART3: It is being used by DOD as the standard MOSA program assessment and rating tool for DOD space system programs.
MOSA OAAT4: Assist U.S. Navy program managers in assessing the “openness” of their programs. It aligns to the Open Architecture Assessment Model (OAAM) as approved by Assistant Secretary of The Navy (ASN) for Research, Development and Acquisition (RDA), which serves as the Navy Acquisition Executive. Other DOD agencies have also been using OAAT since the tool can provide a reproducible and objective method of conducting program assessments.
MOSA KOSS Tool5: One of the key MOSA principles is the Business Principle number 4, namely, Designate Key Interfaces (see Figure 8, B4). The identification of KOSS’s is an important task in realizing open systems. This MOSA principle requires the system designers to compromise between cost and performance by selecting a set of KOSS’s with their associated interfaces that can be assigned widely used open standards allowing for easy and affordable update and frequent refresh. MOSA KOSS tool provides guidance for KOSS’s identification and selection. The tool makes use of system capability road map, system requirements and Subject Matter Expert (SME), program’s sponsor and warfighter knowledge to identify the system/subsystem components expected to have a high volatility over the system life cycle. The tool specifies the key interfaces as those either side of volatile components. The tool will help the satellite system designer to identify and rank KOSS’s components that will meet both programmatic and technical requirements.
This section demonstrates how to use Steps II-A and II-B of the proposed MOSA implementation approach presented in Section 4.4 for the design and build of future resilient and robust satellite systems. Subsections 5.1 and 5.2 present potential modular-and-open satellite Bus and mission PL architectures, respectively.
To demonstrate how to transition the notional modular satellite Bus system architecture presented in Figure 3 to a modular-and-open satellite Bus architecture, this subsection provides an example for the transition of three modular Bus subsystems, namely, BC&DH (Bus Subsystem 3), BTT&C (Bus Subsystem 4) and BEPS (Bus Subsystem 5). These modular Bus subsystems are decomposed to subsystem component-level and analyzed for consideration as potential KOSS’s for open interface standardization. Table 1 summarizes the decomposition and analysis results for these three satellite Bus subsystems.
Modular satellite Bus subsystem component | Modular satellite Bus subsystem and component description | Recommendation for open interface Standardization (potential KOSS) |
---|---|---|
BC&DHS Component No. | Bus Command & Data Handing Subsystem (C&DHS) | |
BC&DHS-1 | Command Authentication Processing Unit (Sync Word Frame Lock, Unparsed Command) | Recommend for Interface standardization |
BC&DHS-2 | System Timing Unit | |
BC&DHS-3 | Fault Management Processing Unit (Execute Stored CMD Sequence, Monitor System Health) | Not recommended for interface standardization due to many variations between systems |
BC&DHS-4 | Bus Resource Management Processing Unit (Managing Internal and External Bus Data) | Recommend for open interface standardization |
BC&DHS-5 | Memory Storage Unit | |
BC&DHS-6 | Spacecraft Control Processor | |
BC&DHS-7 | Bus Telemetry Conditioning Processor | Not required; software driven functions. Should be considered in software interface analysis. |
BC&DHS-8 | Bus Cyber Security Unit | Recommend for open interface standardization |
BTT&CS Component No. | Bus Tracking-Telemetry & Command Subsystem (TT&CS) | |
BTT&CS-1 | TT&C Waveforms/MODEM | Recommend for open interface standardization |
BTT&CS-2 | TT&C Antenna Assembly for S-Band/L-Band | Not recommended for interface standardization. |
BTT&CS-3 | TT&C RF Front-End and Back-End Assembly | Recommend for open interface standardization |
BTT&CS-4 | Unified S-Band (USB) RX/TX Assembly | |
BTT&CS-5 | SGLS S-Band RX/TX Assembly | |
BTT&CS-6 | SGLS Base Band Signal Processing (USB Mode1, 2) | Recommend for open interface standardization |
BTT&CS-7 | In Band TT&C Processor Located at Private Station | Not recommended for interface standardization due to many variations between systems |
BTT&CS-8 | Power Controller Assembly | Recommend for open interface standardization |
BEPS Component No. | Bus Electrical Power Subsystem (EPS) | |
BEPS-1 | Solar Array (SA) | Recommend for open Interface standardization. |
BEPS-2 | Battery Assembly (BA) | Not recommended for interface standardization; Battery size will vary depending on the mission profile. Additional batteries could potentially require customized interfaces to tie all batteries to power bus. |
BEPS-3 | Solar Array Drive Assembly (SADA) | Recommend for open Interface standardization. |
BEPS-4 | Transient Filter Unit (TFU) | Not recommended for interface standardization |
BEPS-5 | Bus Power Regulation Unit (BPRU) | Recommend for open Interface standardization. . |
BEPS-6 | Fuse Box Assembly (FBA) | |
BEPS-7 | Pyro Relay Assembly (PRA) |
Satellite bus subsystems decomposition and potential KOSS.
In practice, the preliminary KOSS analysis results shown in Table 1 should be finalized by the system designer using DOD KOSS tool discussed in Section 4.4. As shown in Table 1, standardizing the BC&DH data interfaces will probably provide the biggest return on investment since the BC&DH subsystem interfaces with each onboard system. Incorporation of the timing interface along with the data interface will minimize the amount of connections, thus reducing overall system mass. Any interfaces that require a significant amount of analysis or Non-Recurring Engineering (NRE) hours is not a good candidate for standardization. The fault management processing interface is in this category, and it is not recommended for standardization.
This subsection provides an example for the transition of the notional modular mission PL architecture presented in Figure 4 to a modular-and-open mission PL architecture. Table 2 summarizes the decomposition and KOSS analysis results for four mission PL subsystems, including PAS (PL Subsystem 1), CPCom-RFS (PL Subsystem 2), PDPS (PL Subsystem 3) and PFTS (PL Subsystem 11).
Modular mission PL subsystem component | Modular mission PL subsystem and component description | Recommendation for open interface standardization (potential KOSS) |
---|---|---|
PAS Component No. | PL Antenna Subsystem (PAS) | |
PAS-1 | PL RF Antenna Configuration (PRAC) | Not recommended for interface standardization due to many variations between systems |
PAS-2 | Beam Forming Unit (BU) | |
PAS-3 | Antenna Controller (AC) | Recommend for Open Interface standardization |
PCom-RFS Component No. | PL Com RF Front-End/Back-End Subsystem (CPCom-RFS) | |
PCom-RFS-1 | PL LNA Component | Not recommended for interface standardization due to many variations between systems/subsystems |
PCom-RFS-2 | PL HPA Component | |
PCom-RFS-3 | Multi-RF Wideband Receiver (RX) | |
PcCm-RFS-4 | PL Up/Down Converters | Recommend for Open Interface standardization |
PCom-RFS-5 | Tunable IF Down Converters | |
PDPS Component No. | PL Digital Processing Subsystem (PDPS) | |
PDPS-1 | PL ADC/DAC | Not recommended for interface standardization due to many variations between systems |
PDPS-2 | FPGA Processor | |
PDPS-3 | PL MOD and DEMO (Optional) | |
PDPS-4 | Digital Network Switch (Optional) | |
PDPS-5 | PL System Controller | |
PTFS Component No. | P/L Frequency and Timing Subsystem (PFTS) | |
PFTS-1 | Atomic Clock Unit (ACU) | Not recommended for interface standardization; ACU and CM&CU will vary depending on mission type and mission requirements |
PFTS-2 | Clock Monitoring & Control Unit (CM&CU) | |
PFTS-3 | Frequency Generation & Up conversion Unit | Recommended for Interface standardization. |
PFTS-4 | Timing Variation and Frequency Stability | Not recommended for interface standardization |
Mission payload subsystems decomposition and potential KOSS.
The mission PL digital processing system is not recommended for interface standardization due to many variations between systems and subsystems. Multi-RF Wideband RX Up/Down Converters and Tunable IF Down Converters require a significant amount of analysis or NRE hours and are also not a good candidate for standardization. Again, DOD KOSS tool should be used to finalize the KOSS analysis results presented here for actual design and build of the satellite systems.
The chapter provides an overview of existing modular satellite Bus and mission PL architectures and associated standards for communication data Busses. The chapter defines open and close interfaces along with industry approved popular standards and discusses the interface design challenges. Moreover, the chapter provides an overview of MOSA and related DOD guidance and assessment tools to address the interface design challenges. Examples for the design and build of modular-and-open satellite Bus and mission PL architectures are also presented. The intent of this chapter is to provide an innovative approach for the satellite system designer to design and build of the next generation satellite achieving a balance between business and technical objectives that make a business sense for both the satellite manufacturers and buyers in terms of lower system acquisition and sustainment costs over its life cycle. The MOSA implementation approach presented here allows the satellite manufacturers to build the satellite Bus and mission PL separately for more production, flexibility, and market competition. Concurrently, the approach also allows the satellite buyers to buy satellite Bus at high volume with reduced unit costs and less schedule risk. Another benefit for the satellite buyer is the adaptability of changing the requirements on the mission PL without impacting the satellite Bus.
Although the preparation of this work was not funded by The Aerospace Corporation, but the author acknowledges the work presented in this chapter was based on his knowledges accumulated over the years from many space programs at The Aerospace Corporation, Raytheon and Jet Propulsion Laboratory. In addition, the author would like to express his appreciation to Aerospace’s manager, Ms. Navneet Mezcciani, for her professional support.
The preparation of this chapter was not funded by the Aerospace Corporation, and it was done by the authors using his own time and resources, thus it does not represent the Aerospace Corporation’s view on the DOD guidance for MOSA implementation and the proposed system architecture solutions.
The author wishes to thank his wife, Thu-Hang Nguyen, for her enormous patience and boundless support during the preparation of this chapter.
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Delac received his B.Sc.E.E. degree in 2003 and is currentlypursuing a Ph.D. degree at the University of Zagreb, Faculty of Electrical Engineering andComputing. His current research interests are digital image analysis, pattern recognition andbiometrics.",institutionString:null,institution:{name:"University of Zagreb",country:{name:"Croatia"}}},{id:"557",title:"Dr.",name:"Andon",middleName:"Venelinov",surname:"Topalov",slug:"andon-topalov",fullName:"Andon Topalov",position:null,profilePictureURL:"https://mts.intechopen.com/storage/users/557/images/1927_n.jpg",biography:"Dr. Andon V. Topalov received the MSc degree in Control Engineering from the Faculty of Information Systems, Technologies, and Automation at Moscow State University of Civil Engineering (MGGU) in 1979. He then received his PhD degree in Control Engineering from the Department of Automation and Remote Control at Moscow State Mining University (MGSU), Moscow, in 1984. From 1985 to 1986, he was a Research Fellow in the Research Institute for Electronic Equipment, ZZU AD, Plovdiv, Bulgaria. In 1986, he joined the Department of Control Systems, Technical University of Sofia at the Plovdiv campus, where he is presently a Full Professor. He has held long-term visiting Professor/Scholar positions at various institutions in South Korea, Turkey, Mexico, Greece, Belgium, UK, and Germany. And he has coauthored one book and authored or coauthored more than 80 research papers in conference proceedings and journals. 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We conclude this chapter by expressing personal perspective on the probable challenges and developments of the controllable synthesis of CeO2 nanomaterials for various applications.",book:{id:"5510",slug:"functionalized-nanomaterials",title:"Functionalized Nanomaterials",fullTitle:"Functionalized Nanomaterials"},signatures:"Adnan Younis, Dewei Chu and Sean Li",authors:[{id:"191574",title:"Dr.",name:"Adnan",middleName:null,surname:"Younis",slug:"adnan-younis",fullName:"Adnan Younis"}]}],mostDownloadedChaptersLast30Days:[{id:"38951",title:"Carbon Nanotube Transparent Electrode",slug:"carbon-nanotube-transparent-electrode",totalDownloads:3985,totalCrossrefCites:3,totalDimensionsCites:5,abstract:null,book:{id:"3077",slug:"syntheses-and-applications-of-carbon-nanotubes-and-their-composites",title:"Syntheses and Applications of Carbon Nanotubes and Their Composites",fullTitle:"Syntheses and Applications of Carbon Nanotubes and Their Composites"},signatures:"Jing Sun and Ranran Wang",authors:[{id:"153508",title:"Prof.",name:"Jing",middleName:null,surname:"Sun",slug:"jing-sun",fullName:"Jing Sun"},{id:"153596",title:"Ms.",name:"Ranran",middleName:null,surname:"Wang",slug:"ranran-wang",fullName:"Ranran Wang"}]},{id:"49413",title:"Electrodeposition of Nanostructure Materials",slug:"electrodeposition-of-nanostructure-materials",totalDownloads:3733,totalCrossrefCites:1,totalDimensionsCites:7,abstract:"We are conducting a multi-disciplinary research work that involves development of nanostructured thin films of semiconductors for different applications. Nanotechnology is widely considered to constitute the basis of the next technological revolution, following on from the first Industrial Revolution, which began around 1750 with the introduction of the steam engine and steelmaking. Nanotechnology is defined as the design, characterization, production, and application of materials, devices and systems by controlling shape and size of the nanoscale. The nanoscale itself is at present considered to cover the range from 1 to 100 nm. All samples prepared in thin film forms and the characterization revealed their nanostructure. The major exploitation of thin films has been in microelectronics, there are numerous and growing applications in communications, optical electronics, coatings of all kinds, and in energy generation. A great many sophisticated analytical instruments and techniques, largely developed to characterize thin films, have already become indispensable in virtually every scientific endeavor irrespective of discipline. Among all these techniques, electrodeposition is the most suitable technique for nanostructured thin films from aqueous solution served as samples under investigation. The electrodeposition of metallic layers from aqueous solution is based on the discharge of metal ions present in the electrolyte at a cathodic surface (the substrate or component.) The metal ions accept an electron from the electrically conducting material at the solid- electrolyte interface and then deposit as metal atoms onto the surface. The electrons necessary for this to occur are either supplied from an externally applied potential source or are surrendered by a reducing agent present in solution (electroless reduction). The metal ions themselves derive either from metal salts added to solution, or by the anodic dissolution of the so-called sacrificial anodes, made of the same metal that is to be deposited at the cathode.",book:{id:"4718",slug:"electroplating-of-nanostructures",title:"Electroplating of Nanostructures",fullTitle:"Electroplating of Nanostructures"},signatures:"Souad A. M. Al-Bat’hi",authors:[{id:"174793",title:"Dr.",name:"Mohamad",middleName:null,surname:"Souad",slug:"mohamad-souad",fullName:"Mohamad Souad"}]},{id:"54226",title:"Localized Surface Plasmon Resonance for Optical Fiber-Sensing Applications",slug:"localized-surface-plasmon-resonance-for-optical-fiber-sensing-applications",totalDownloads:2265,totalCrossrefCites:2,totalDimensionsCites:5,abstract:"It is well known that optical fiber sensors have attracted the attention of scientific community due to its intrinsic advantages, such as lightweight, small size, portability, remote sensing, immunity to electromagnetic interferences and the possibility of multiplexing several signals. This field has shown a dramatic growth thanks to the creation of sensitive thin films onto diverse optical fiber configurations. In this sense, a wide range of optical fiber devices have been successfully fabricated for monitoring biological, chemical, medical or physical parameters. In addition, the use of nanoparticles into the sensitive thin films has resulted in an enhancement in the response time, robustness or sensitivity in the optical devices, which is associated to the inherent properties of nanoparticles (high surface area ratio or porosity). Among all of them, the metallic nanoparticles are of great interest for sensing applications due to the presence of strong absorption bands in the visible and near-infrared regions, due to their localized surface plasmon resonances (LSPR). These optical resonances are due to the coupling of certain modes of the incident light to the collective oscillation of the conduction electrons of the metallic nanoparticles. The LSPR extinction bands are very useful for sensing applications as far as they can be affected by refractive index variations of the surrounding medium of the nanoparticles, and therefore, it is possible to create optical sensors with outstanding properties such as high sensitivity and optical self-reference. In this chapter, the attractive optical properties of metal nanostructures and their implementation into different optical fiber configuration for sensing or biosensing applications will be studied.",book:{id:"5721",slug:"nanoplasmonics-fundamentals-and-applications",title:"Nanoplasmonics",fullTitle:"Nanoplasmonics - Fundamentals and Applications"},signatures:"Pedro J. Rivero, Javier Goicoechea and Francisco J. Arregui",authors:[{id:"69816",title:"Dr.",name:"Javier",middleName:null,surname:"Goicoechea",slug:"javier-goicoechea",fullName:"Javier Goicoechea"},{id:"188796",title:"Dr.",name:"Pedro J.",middleName:null,surname:"Rivero",slug:"pedro-j.-rivero",fullName:"Pedro J. 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Piezoelectric materials are capable of transforming mechanical strain and vibration energy into electrical energy. This property allows opportunities for implementing renewable and sustainable energy through power harvesting and self-sustained smart sensing in buildings. As the most common construction material, plain cement paste lacks satisfactory piezoelectricity and is not efficient at harvesting the electrical energy from the ambient vibrations of a building system. In recent years, many techniques have been proposed and applied to improve the piezoelectric capacity of cement-based composite, namely admixture incorporation and physical. The successful application of piezoelectric materials for sustainable building development not only relies on understanding the mechanism of the piezoelectric properties of various building components, but also the latest developments and implementations in the building industry. Therefore, this review systematically illustrates research efforts to develop new construction materials with high piezoelectricity and energy storage capacity. In addition, this article discusses the latest techniques for utilizing the piezoelectric materials in energy harvesters, sensors and actuators for various building systems. With advanced methods for improving the cementations piezoelectricity and applying the material piezoelectricity for different building functions, more renewable and sustainable building systems are anticipated.",book:{id:"10511",slug:"multifunctional-ferroelectric-materials",title:"Multifunctional Ferroelectric Materials",fullTitle:"Multifunctional Ferroelectric Materials"},signatures:"B. Chandra Sekhar, B. Dhanalakshmi, B. Srinivasa Rao, S. Ramesh, K. Venkata Prasad, P.S.V. Subba Rao and B. Parvatheeswara Rao",authors:[{id:"335022",title:"Dr.",name:"B. Chandra",middleName:null,surname:"Sekhar",slug:"b.-chandra-sekhar",fullName:"B. Chandra Sekhar"},{id:"422021",title:"Dr.",name:"B.",middleName:null,surname:"Dhanalakshmi",slug:"b.-dhanalakshmi",fullName:"B. Dhanalakshmi"},{id:"422022",title:"Dr.",name:"B.Srinivasa",middleName:null,surname:"Rao",slug:"b.srinivasa-rao",fullName:"B.Srinivasa Rao"},{id:"422023",title:"Dr.",name:"S.",middleName:null,surname:"Ramesh",slug:"s.-ramesh",fullName:"S. Ramesh"},{id:"422024",title:"Dr.",name:"K.Venkata",middleName:null,surname:"Prasad",slug:"k.venkata-prasad",fullName:"K.Venkata Prasad"},{id:"422025",title:"Dr.",name:"P.S.V",middleName:null,surname:"Subba Rao",slug:"p.s.v-subba-rao",fullName:"P.S.V Subba Rao"},{id:"422026",title:"Dr.",name:"B.Parvatheeswara",middleName:null,surname:"Rao",slug:"b.parvatheeswara-rao",fullName:"B.Parvatheeswara Rao"}]}],onlineFirstChaptersFilter:{topicId:"1169",limit:6,offset:0},onlineFirstChaptersCollection:[{id:"81438",title:"Research Progress of Ionic Thermoelectric Materials for Energy Harvesting",slug:"research-progress-of-ionic-thermoelectric-materials-for-energy-harvesting",totalDownloads:24,totalDimensionsCites:0,doi:"10.5772/intechopen.101771",abstract:"Thermoelectric material is a kind of functional material that can mutually convert heat energy and electric energy. It can convert low-grade heat energy (less than 130°C) into electric energy. Compared with traditional electronic thermoelectric materials, ionic thermoelectric materials have higher performance. The Seebeck coefficient can generate 2–3 orders of magnitude higher ionic thermoelectric potential than electronic thermoelectric materials, so it has good application prospects in small thermoelectric generators and solar power generation. According to the thermoelectric conversion mechanism, ionic thermoelectric materials can be divided into ionic thermoelectric materials based on the Soret effect and thermocouple effect. They are widely used in pyrogen batteries and ionic thermoelectric capacitors. The latest two types of ionic thermoelectric materials are in this article. The research progress is explained, and the problems and challenges of ionic thermoelectric materials and the future development direction are also put forward.",book:{id:"10037",title:"Thermoelectricity - Recent Advances, New Perspectives and Applications",coverURL:"https://cdn.intechopen.com/books/images_new/10037.jpg"},signatures:"Jianwei Zhang, Ying Xiao, Bowei Lei, Gengyuan Liang and Wenshu Zhao"},{id:"77670",title:"Thermoelectric Elements with Negative Temperature Factor of Resistance",slug:"thermoelectric-elements-with-negative-temperature-factor-of-resistance",totalDownloads:72,totalDimensionsCites:0,doi:"10.5772/intechopen.98860",abstract:"The method of manufacturing of ceramic materials on the basis of ferrites of nickel and cobalt by synthesis and sintering in controllable regenerative atmosphere is presented. As the generator of regenerative atmosphere the method of conversion of carbonic gas is offered. Calculation of regenerative atmosphere for simultaneous sintering of ceramic ferrites of nickel and cobalt is carried out. It is offered, methods of the dilated nonequilibrium thermodynamics to view process of distribution of a charge and heat along a thermoelement branch. The model of a thermoelement taking into account various relaxation times of a charge and warmth is constructed.",book:{id:"10037",title:"Thermoelectricity - Recent Advances, New Perspectives and Applications",coverURL:"https://cdn.intechopen.com/books/images_new/10037.jpg"},signatures:"Yuri Bokhan"},{id:"79236",title:"Processing Techniques with Heating Conditions for Multiferroic Systems of BiFeO3, BaTiO3, PbTiO3, CaTiO3 Thin Films",slug:"processing-techniques-with-heating-conditions-for-multiferroic-systems-of-bifeo3-batio3-pbtio3-catio",totalDownloads:96,totalDimensionsCites:0,doi:"10.5772/intechopen.101122",abstract:"In this chapter, we have report a list of synthesis methods (including both synthesis steps & heating conditions) used for thin film fabrication of perovskite ABO3 (BiFeO3, BaTiO3, PbTiO3 and CaTiO3) based multiferroics (in both single-phase and composite materials). The processing of high quality multiferroic thin film have some features like epitaxial strain, physical phenomenon at atomic-level, interfacial coupling parameters to enhance device performance. Since these multiferroic thin films have ME properties such as electrical (dielectric, magnetoelectric coefficient & MC) and magnetic (ferromagnetic, magnetic susceptibility etc.) are heat sensitive, i.e. ME response at low as well as higher temperature might to enhance the device performance respect with long range ordering. The magnetoelectric coupling between ferromagnetism and ferroelectricity in multiferroic becomes suitable in the application of spintronics, memory and logic devices, and microelectronic memory or piezoelectric devices. In comparison with bulk multiferroic, the fabrication of multiferroic thin film with different structural geometries on substrate has reducible clamping effect. A brief procedure for multiferroic thin film fabrication in terms of their thermal conditions (temperature for film processing and annealing for crystallization) are described. Each synthesis methods have its own characteristic phenomenon in terms of film thickness, defects formation, crack free film, density, chip size, easier steps and availability etc. been described. A brief study towards phase structure and ME coupling for each multiferroic system of BiFeO3, BaTiO3, PbTiO3 and CaTiO3 is shown.",book:{id:"10037",title:"Thermoelectricity - Recent Advances, New Perspectives and Applications",coverURL:"https://cdn.intechopen.com/books/images_new/10037.jpg"},signatures:"Kuldeep Chand Verma and Manpreet Singh"},{id:"78034",title:"Quantum Physical Interpretation of Thermoelectric Properties of Ruthenate Pyrochlores",slug:"quantum-physical-interpretation-of-thermoelectric-properties-of-ruthenate-pyrochlores",totalDownloads:78,totalDimensionsCites:0,doi:"10.5772/intechopen.99260",abstract:"Lead- and lead-yttrium ruthenate pyrochlores were synthesized and investigated for Seebeck coefficients, electrical- and thermal conductivity. Compounds A2B2O6.5+z with 0 ≤ z < 0.5 were defect pyrochlores and p-type conductors. The thermoelectric data were analyzed using quantum physical models to identify scattering mechanisms underlying electrical (σ) and thermal conductivity (κ) and to understand the temperature dependence of the Seebeck effect (S). In the metal-like lead ruthenates with different Pb:Ru ratios, σ (T) and the electronic thermal conductivity κe (T) were governed by ‘electron impurity scattering’, the lattice thermal conductivity κL (T) by the 3-phonon resistive process (Umklapp scattering). In the lead-yttrium ruthenate solid solutions (Pb(2-x)YxRu2O(6.5±z)), a metal–insulator transition occurred at 0.2 moles of yttrium. On the metallic side (<0.2 moles Y) ‘electron impurity scattering’ prevailed. On the semiconductor/insulator side between x = 0.2 and x = 1.0 several mechanisms were equally likely. At x > 1.5 the Mott Variable Range Hopping mechanism was active. S (T) was discussed for Pb-Y-Ru pyrochlores in terms of the effect of minority carrier excitation at lower- and a broadening of the Fermi distribution at higher temperatures. The figures of merit of all of these pyrochlores were still small (≤7.3 × 10−3).",book:{id:"10037",title:"Thermoelectricity - Recent Advances, New Perspectives and Applications",coverURL:"https://cdn.intechopen.com/books/images_new/10037.jpg"},signatures:"Sepideh Akhbarifar"},{id:"77635",title:"Optimization of Thermoelectric Properties Based on Rashba Spin Splitting",slug:"optimization-of-thermoelectric-properties-based-on-rashba-spin-splitting",totalDownloads:124,totalDimensionsCites:0,doi:"10.5772/intechopen.98788",abstract:"In recent years, the application of thermoelectricity has become more and more widespread. Thermoelectric materials provide a simple and environmentally friendly solution for the direct conversion of heat to electricity. The development of higher performance thermoelectric materials and their performance optimization have become more important. Generally, to improve the ZT value, electrical conductivity, Seebeck coefficient and thermal conductivity must be globally optimized as a whole object. However, due to the strong coupling among ZT parameters in many cases, it is very challenging to break the bottleneck of ZT optimization currently. Beyond the traditional optimization methods (such as inducing defects, varying temperature), the Rashba effect is expected to effectively increase the S2σ and decrease the κ, thus enhancing thermoelectric performance, which provides a new strategy to develop new-generation thermoelectric materials. Although the Rashba effect has great potential in enhancing thermoelectric performance, the underlying mechanism of Rashba-type thermoelectric materials needs further research. In addition, how to introduce Rashba spin splitting into current thermoelectric materials is also of great significance to the optimization of thermoelectricity.",book:{id:"10037",title:"Thermoelectricity - Recent Advances, New Perspectives and Applications",coverURL:"https://cdn.intechopen.com/books/images_new/10037.jpg"},signatures:"Zhenzhen Qin"},{id:"75364",title:"Challenges in Improving Performance of Oxide Thermoelectrics Using Defect Engineering",slug:"challenges-in-improving-performance-of-oxide-thermoelectrics-using-defect-engineering",totalDownloads:214,totalDimensionsCites:0,doi:"10.5772/intechopen.96278",abstract:"Oxide thermoelectric materials are considered promising for high-temperature thermoelectric applications in terms of low cost, temperature stability, reversible reaction, and so on. Oxide materials have been intensively studied to suppress the defects and electronic charge carriers for many electronic device applications, but the studies with a high concentration of defects are limited. It desires to improve thermoelectric performance by enhancing its charge transport and lowering its lattice thermal conductivity. For this purpose, here, we modified the stoichiometry of cation and anion vacancies in two different systems to regulate the carrier concentration and explored their thermoelectric properties. Both cation and anion vacancies act as a donor of charge carriers and act as phonon scattering centers, decoupling the electrical conductivity and thermal conductivity.",book:{id:"10037",title:"Thermoelectricity - Recent Advances, New Perspectives and Applications",coverURL:"https://cdn.intechopen.com/books/images_new/10037.jpg"},signatures:"Jamil Ur Rahman, Gul Rahman and Soonil Lee"}],onlineFirstChaptersTotal:6},preDownload:{success:null,errors:{}},subscriptionForm:{success:null,errors:{}},aboutIntechopen:{},privacyPolicy:{},peerReviewing:{},howOpenAccessPublishingWithIntechopenWorks:{},sponsorshipBooks:{sponsorshipBooks:[],offset:8,limit:8,total:0},allSeries:{pteSeriesList:[{id:"14",title:"Artificial Intelligence",numberOfPublishedBooks:9,numberOfPublishedChapters:87,numberOfOpenTopics:6,numberOfUpcomingTopics:0,issn:"2633-1403",doi:"10.5772/intechopen.79920",isOpenForSubmission:!0},{id:"7",title:"Biomedical Engineering",numberOfPublishedBooks:12,numberOfPublishedChapters:98,numberOfOpenTopics:3,numberOfUpcomingTopics:0,issn:"2631-5343",doi:"10.5772/intechopen.71985",isOpenForSubmission:!0}],lsSeriesList:[{id:"11",title:"Biochemistry",numberOfPublishedBooks:27,numberOfPublishedChapters:287,numberOfOpenTopics:4,numberOfUpcomingTopics:0,issn:"2632-0983",doi:"10.5772/intechopen.72877",isOpenForSubmission:!0},{id:"25",title:"Environmental Sciences",numberOfPublishedBooks:1,numberOfPublishedChapters:9,numberOfOpenTopics:4,numberOfUpcomingTopics:0,issn:"2754-6713",doi:"10.5772/intechopen.100362",isOpenForSubmission:!0},{id:"10",title:"Physiology",numberOfPublishedBooks:11,numberOfPublishedChapters:139,numberOfOpenTopics:4,numberOfUpcomingTopics:0,issn:"2631-8261",doi:"10.5772/intechopen.72796",isOpenForSubmission:!0}],hsSeriesList:[{id:"3",title:"Dentistry",numberOfPublishedBooks:8,numberOfPublishedChapters:129,numberOfOpenTopics:0,numberOfUpcomingTopics:2,issn:"2631-6218",doi:"10.5772/intechopen.71199",isOpenForSubmission:!1},{id:"6",title:"Infectious Diseases",numberOfPublishedBooks:13,numberOfPublishedChapters:107,numberOfOpenTopics:3,numberOfUpcomingTopics:1,issn:"2631-6188",doi:"10.5772/intechopen.71852",isOpenForSubmission:!0},{id:"13",title:"Veterinary Medicine and Science",numberOfPublishedBooks:10,numberOfPublishedChapters:103,numberOfOpenTopics:3,numberOfUpcomingTopics:0,issn:"2632-0517",doi:"10.5772/intechopen.73681",isOpenForSubmission:!0}],sshSeriesList:[{id:"22",title:"Business, Management and Economics",numberOfPublishedBooks:1,numberOfPublishedChapters:12,numberOfOpenTopics:2,numberOfUpcomingTopics:1,issn:null,doi:"10.5772/intechopen.100359",isOpenForSubmission:!0},{id:"23",title:"Education and Human Development",numberOfPublishedBooks:0,numberOfPublishedChapters:0,numberOfOpenTopics:2,numberOfUpcomingTopics:0,issn:null,doi:"10.5772/intechopen.100360",isOpenForSubmission:!1},{id:"24",title:"Sustainable Development",numberOfPublishedBooks:0,numberOfPublishedChapters:10,numberOfOpenTopics:4,numberOfUpcomingTopics:1,issn:null,doi:"10.5772/intechopen.100361",isOpenForSubmission:!0}],testimonialsList:[{id:"6",text:"It is great to work with the IntechOpen to produce a worthwhile collection of research that also becomes a great educational resource and guide for future research endeavors.",author:{id:"259298",name:"Edward",surname:"Narayan",institutionString:null,profilePictureURL:"https://mts.intechopen.com/storage/users/259298/images/system/259298.jpeg",slug:"edward-narayan",institution:{id:"3",name:"University of Queensland",country:{id:null,name:"Australia"}}}},{id:"13",text:"The collaboration with and support of the technical staff of IntechOpen is fantastic. The whole process of submitting an article and editing of the submitted article goes extremely smooth and fast, the number of reads and downloads of chapters is high, and the contributions are also frequently cited.",author:{id:"55578",name:"Antonio",surname:"Jurado-Navas",institutionString:null,profilePictureURL:"https://s3.us-east-1.amazonaws.com/intech-files/0030O00002bRisIQAS/Profile_Picture_1626166543950",slug:"antonio-jurado-navas",institution:{id:"720",name:"University of Malaga",country:{id:null,name:"Spain"}}}}]},series:{item:{id:"22",title:"Business, Management and Economics",doi:"10.5772/intechopen.100359",issn:null,scope:"\r\n\tThis series will provide a comprehensive overview of recent research trends in business and management, economics, and marketing. 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",coverUrl:"https://cdn.intechopen.com/series/covers/22.jpg",latestPublicationDate:"May 18th, 2022",hasOnlineFirst:!0,numberOfPublishedBooks:1,editor:{id:"356540",title:"Prof.",name:"Taufiq",middleName:null,surname:"Choudhry",slug:"taufiq-choudhry",fullName:"Taufiq Choudhry",profilePictureURL:"https://s3.us-east-1.amazonaws.com/intech-files/0033Y000036X2hvQAC/Profile_Picture_2022-03-14T08:58:03.jpg",biography:"Prof. Choudhry holds a BSc degree in Economics from the University of Iowa, as well as a Masters and Ph.D. in Applied Economics from Clemson University, USA. In January 2006, he became a Professor of Finance at the University of Southampton Business School. He was previously a Professor of Finance at the University of Bradford Management School. He has over 80 articles published in international finance and economics journals. His research interests and specialties include financial econometrics, financial economics, international economics and finance, housing markets, financial markets, among others.",institutionString:null,institution:{name:"University of Southampton",institutionURL:null,country:{name:"United Kingdom"}}},editorTwo:null,editorThree:null},subseries:{paginationCount:3,paginationItems:[{id:"86",title:"Business and Management",coverUrl:"https://cdn.intechopen.com/series_topics/covers/86.jpg",isOpenForSubmission:!0,editor:{id:"128342",title:"Prof.",name:"Vito",middleName:null,surname:"Bobek",slug:"vito-bobek",fullName:"Vito Bobek",profilePictureURL:"https://mts.intechopen.com/storage/users/128342/images/system/128342.jpg",biography:"Dr. Vito Bobek works as an international management professor at the University of Applied Sciences FH Joanneum, Graz, Austria. He has published more than 400 works in his academic career and visited twenty-two universities worldwide as a visiting professor. Dr. Bobek is a member of the editorial boards of six international journals and a member of the Strategic Council of the Minister of Foreign Affairs of the Republic of Slovenia. He has a long history in academia, consulting, and entrepreneurship. His own consulting firm, Palemid, has managed twenty significant projects, such as Cooperation Program Interreg V-A (Slovenia-Austria) and Capacity Building for the Serbian Chamber of Enforcement Agents. He has also participated in many international projects in Italy, Germany, Great Britain, the United States, Spain, Turkey, France, Romania, Croatia, Montenegro, Malaysia, and China. Dr. Bobek is also a co-founder of the Academy of Regional Management in Slovenia.",institutionString:"Universities of Applied Sciences FH Joanneum, Austria",institution:null},editorTwo:{id:"293992",title:"Dr.",name:"Tatjana",middleName:null,surname:"Horvat",slug:"tatjana-horvat",fullName:"Tatjana Horvat",profilePictureURL:"https://s3.us-east-1.amazonaws.com/intech-files/0030O00002hXb0hQAC/Profile_Picture_1642419002203",biography:"Tatjana Horvat works as a professor for accountant and auditing at the University of Primorska, Slovenia. She is a Certified State Internal Auditor (licensed by Ministry of Finance RS) and Certified Internal Auditor for Business Sector and Certified accountant (licensed by Slovenian Institute of Auditors). At the Ministry of Justice of Slovenia, she is a member of examination boards for court expert candidates and judicial appraisers in the following areas: economy/finance, valuation of companies, banking, and forensic investigation of economic operations/accounting. At the leading business newspaper Finance in Slovenia (Swedish ownership), she is the editor and head of the area for business, finance, tax-related articles, and educational programs.",institutionString:null,institution:{name:"University of Primorska",institutionURL:null,country:{name:"Slovenia"}}},editorThree:null},{id:"87",title:"Economics",coverUrl:"https://cdn.intechopen.com/series_topics/covers/87.jpg",isOpenForSubmission:!0,editor:{id:"327730",title:"Prof.",name:"Jaime",middleName:null,surname:"Ortiz",slug:"jaime-ortiz",fullName:"Jaime Ortiz",profilePictureURL:"https://s3.us-east-1.amazonaws.com/intech-files/0033Y00002zaOKZQA2/Profile_Picture_1642145584421",biography:"Dr. Jaime Ortiz holds degrees from Chile, the Netherlands, and the United States. He has held tenured faculty, distinguished professorship, and executive leadership appointments in several universities around the world. Dr. Ortiz has previously worked for international organizations and non-government entities in economic and business matters, and he has university-wide globalization engagement in more than thirty-six countries. He has advised, among others, the United Nations Development Program, Inter-American Development Bank, Organization of American States, Pre-investment Organization of Latin America and the Caribbean, Technical Cooperation of the Suisse Government, and the World Bank. Dr. Ortiz is the author, co-author, or editor of books, book chapters, textbooks, research monographs and technical reports, and refereed journal articles. He is listed in Who’s Who in the World, Who’s Who in America, Who’s Who in Finance and Business, Who’s Who in Business Higher Education, Who’s Who in American Education, and Who’s Who Directory of Economists. Dr. Ortiz has been a Fulbright Scholar and an MSI Leadership Fellow with the W.K. Kellogg Foundation. His teaching interests revolve around global economies and markets while his research focuses on topics related to development and growth, global business decisions, and the economics of technical innovation.",institutionString:null,institution:{name:"University of Houston",institutionURL:null,country:{name:"United States of America"}}},editorTwo:null,editorThree:null},{id:"88",title:"Marketing",coverUrl:"https://cdn.intechopen.com/series_topics/covers/88.jpg",isOpenForSubmission:!1,editor:null,editorTwo:null,editorThree:null}]},overviewPageOFChapters:{paginationCount:1,paginationItems:[{id:"81831",title:"Deep Network Model and Regression Analysis using OLS Method for Predicting Lung Vital Capacity",doi:"10.5772/intechopen.104737",signatures:"Harun Sümbül",slug:"deep-network-model-and-regression-analysis-using-ols-method-for-predicting-lung-vital-capacity",totalDownloads:2,totalCrossrefCites:0,totalDimensionsCites:0,authors:null,book:{title:"Decision Science - Recent Advances and Applications",coverURL:"https://cdn.intechopen.com/books/images_new/11604.jpg",subseries:{id:"86",title:"Business and Management"}}}]},overviewPagePublishedBooks:{paginationCount:1,paginationItems:[{type:"book",id:"11392",title:"Leadership in a Changing World",subtitle:"A Multidimensional Perspective",coverURL:"https://cdn.intechopen.com/books/images_new/11392.jpg",slug:"leadership-in-a-changing-world-a-multidimensional-perspective",publishedDate:"May 11th 2022",editedByType:"Edited by",bookSignature:"Muhammad Mohiuddin, Bilal Khalid, Md. Samim Al Azad and Slimane Ed-dafali",hash:"86a6d33cf601587e591064ce92effc02",volumeInSeries:1,fullTitle:"Leadership in a Changing World - A Multidimensional Perspective",editors:[{id:"418514",title:"Dr.",name:"Muhammad",middleName:null,surname:"Mohiuddin",slug:"muhammad-mohiuddin",fullName:"Muhammad Mohiuddin",profilePictureURL:"https://s3.us-east-1.amazonaws.com/intech-files/0033Y000038UqSfQAK/Profile_Picture_2022-05-13T10:39:03.jpg",biography:"Dr. Muhammad Mohiuddin is an Associate Professor of International Business at Laval University, Canada. He has taught at Thompson Rivers University, Canada; University of Paris-Est, France; Osnabruck University of Applied Science, Germany; and Shanghai Institute of Technology and Tianjin University of Technology, China. He has published research in Research Policy, Applied Economics, Review of Economic Philosophy, Strategic Change, International Journal of Logistics, Sustainability, Journal of Environmental Management, Journal of Global Information Management, Journal of Cleaner Production, M@N@GEMENT, and more. He is a member of CEDIMES Institut (France), Academy of International Business (AIB), Strategic Management Society (SMS), Academy of Management (AOM), Administrative Science Association of Canada (ASAC), and Canadian council of small business and entrepreneurship (CCSBE). He is currently the director of the Research Group on Contemporary Asia (GERAC) at Laval University. 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