This chapter describes the development and application of sliding-mode fault-tolerant controlFault Tolerant Control schemes to safety critical aerospace scenarios. There is growing literature exploiting the specific and unique properties of sliding modes in the field of fault-tolerant controlFault Tolerant Control, but many of the results are more theoretical in nature, and relatively little work has been published describing real implementations of these ideas. This chapter focuses on the development of fault-tolerant sliding-mode controllers for a class of linear parameter varyingLinear Parameter Varying systems. This class of systems is commonly employed to model different aerospace systems, and so represents a natural starting point for these developments. The chapter describes the implementation of these ideas on a small, unmanned quadrotorQuadrotor UAVUnmanned Aerial Vehicle (UAV), and also piloted flight tests on a full-scale twin-engine civil aircraft.
Flight Evaluation of a Sliding-Mode Fault-Tolerant Control Scheme
Studies in Systems, Decision and Control
01.11.2023
42 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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