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Document type:
Konferenzbeitrag 
Author(s):
Zhang, Fubiao; Holzapfel, Florian 
Title:
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...    »
 
Book / Congress title:
AIAA Guidance, Navigation, and Control Conference 
Year:
2015 
Covered by:
Scopus; Web of Science 
Fulltext / DOI: