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Reconfiguration Control Design of UAV against Actuator Faults Based on Control Allocation Method

The paper concentrates on the problem of fault-tolerant control of UAV against actuator faults from the perspective of flight control system architecture. Using backstepping control method and inverse optimization theory, the design of backstepping optimal control law was constructed. Based on the f...

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Sonraí bibleagrafaíochta
Príomhchruthaitheoirí: Yuwei Cui, Aijun Li, Biao Duan, Shabbir Wasif
Formáid: Artigo
Teanga:Inglês
Foilsithe / Cruthaithe: Wiley 2022-01-01
Sraith:International Journal of Aerospace Engineering
Rochtain ar líne:http://dx.doi.org/10.1155/2022/4481553
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