Chapters authored
Adaptive Integral High‐Order Sliding Mode for a Fixed Wing Aircraft
In order to develop and implement the laws piloting for an aircraft, flights validation will be necessary. This could in fact be done, in a first step, by using flight simulators. In this work, we choose the predator virtual model flying in MicrosoftTM flight simulator (MSFS) and we propose the procedure of controlling its attitude. We send the adaptive integral high‐order sliding mode (AIHOSM) inputs piloting control. This work is a real‐time virtual simulation. For the AIHOSM controller, we propose the gain adaptation for reduction of chattering phenomena and possibility to control the aircraft presented by the uncertain nonlinear systems in which the uncertainties have unknown bounds. This technique is more robust and simpler to implement than the quaternion one and only needs the information about the sliding mode surface.
Part of the book: Recent Developments in Sliding Mode Control