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Dokumenttyp:
Konferenzbeitrag 
Autor(en):
Zhang, Fubiao; Holzapfel, Florian 
Titel:
Flight Control Using Physical Dynamic Inversion 
Abstract:
This paper presents a new architecture of dynamic inversion based flight control law, which decouples desired dynamics specification and stabilizing feedback controller design. The decoupling is achieved by using a physically integrated reference model, which mimics desired aircraft response, and an incrementally cascaded error controller, which shapes the extra dynamics beyond the desired dynamics. This approach makes best use of flight dynamics both in feed forward and feedback design, in an a...    »
 
Kongress- / Buchtitel:
AIAA Guidance, Navigation, and Control Conference 
Jahr:
2015 
Nachgewiesen in:
Scopus; Web of Science