NDLI: Visual simulation research of post-stall maneuverability flight control laws based on Matlab/Flightgear/Atlas

Content Provider	IEEE Xplore Digital Library
Author	Cen Fei Sun Hai-Sheng Liu Zhi-Tao Nie Bo-Wen
Copyright Year	2012
Description	Author affiliation: China Aerodynamics Research &Development Center, Mianyang 621000 (Cen Fei; Sun Hai-Sheng; Liu Zhi-Tao; Nie Bo-Wen)
Abstract	Flight simulation is a necessary process in designing of flight control laws, so develop a convenient and low cost flight simulator is very important and meaningful, especially in the early design stage of control law design. This paper develops a real time visualization flight simulator based on Matlab/Flightgear/Atlas, and uses nonlinear dynamic inversion method combined with flight quality requirements to design flight control laws for a supermaneuverable aircraft. It puts forward the cobra maneuver simulation on the flight simulator 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 and validate the feasibility of the flight simulator.
Starting Page	607
Ending Page	612
File Size	779510
Page Count	6
File Format	PDF
ISBN	9781467325813
ISSN	21612927
e-ISBN	9789881563811
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2012-07-25
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Chinese Assoc of Automati
Subject Keyword	Visualization flight simulation flightgear flight control Aerospace simulation Electronic mail Nonlinear dynamical systems post-stall maneuverability MATLAB nonlinear dynamic inversion Aerospace control
Content Type	Text
Resource Type	Article

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