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Fault-tolerant flight control for a fixed-wing unmanned aerial vehicle with partial horizontal and vertical stabiliser losses
(Stellenbosch : Stellenbosch University, 2016-12)ENGLISH ABSTRACT: In the study reported here, a fault-tolerant flight control system for a fixed-wing unmanned aerial vehicle with partial stabiliser loss is designed, analysed, implemented and verified. The partial ... -
Optimised active fault detection for an open loop stable system
(Stellenbosch : Stellenbosch University, 2016-12)Active fault detection for a stable open-loop linear time invariant system is considered. The optimal active fault detection setup is developed around an estimator based architecture. The auxiliary signal and estimator are ...