NDLI: Design and evaluation of a post-stall maneuverable flight control law based on nonlinear dynamic inversion

Content Provider	IEEE Xplore Digital Library
Author	Cen Fei Sun Hai-Sheng Liang Pin
Copyright Year	2011
Description	Author affiliation: China Aerodynamics Research & Development Center, Mianyang 621000, China (Cen Fei; Sun Hai-Sheng; Liang Pin)
Abstract	The paper uses nonlinear dynamic inversion combined with flight quality requirements to design flight control laws for a supermaneuverable aircraft, and introduces a new control allocation strategy in combination of aero control surfaces and thrust vectoring based on daisy-chaining algorithm and least-energy method. After Optimizing the configuration and parameters of the control laws, it uses several paragraphs to take robust analyse and Evaluation, with the employing of Bode diagram and Neal-Smith standard. It puts forward the cobra maneuver simulation with a 3D display at last. The simulation results show that the control laws perform excellently not only at the normal flight envelope but also at high angle of attack.
Starting Page	293
Ending Page	298
File Size	722144
Page Count	6
File Format	PDF
ISBN	9781457706776
ISSN	21612927
e-ISBN	9789881725592
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2011-07-22
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Chinese Assoc of Automati
Subject Keyword	NASA Flight Control Aerodynamics Post-stall Maneuver Three dimensional displays Robustness Nonlinear Dynamic Inversion Nonlinear dynamical systems Electronic mail Flight Quality Aerospace control
Content Type	Text
Resource Type	Article

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