The synthesis of MIMO fault-tolerant control systems under control failures is considered. The solution is written in an analytical form, which makes it possible to synthesize simplified circuit implementations and adjust coefficients of the fault-tolerant control system in the case of a non-stationary object. А nonlinear medium-range aircraft model was used to verify the results.
Aircraft control law reconfiguration
2015
Aufsatz (Zeitschrift)
Elektronische Ressource
Unbekannt
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