DocumentCode
581612
Title
Visual simulation research of post-stall maneuverability flight control laws based on Matlab/Flightgear/Atlas
Author
Fei, Cen ; Hai-sheng, Sun ; Zhi-tao, Liu ; Bo-wen, Nie
Author_Institution
China Aerodynamics R&D Center, Mianyang, China
fYear
2012
fDate
25-27 July 2012
Firstpage
607
Lastpage
612
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.
Keywords
aerospace computing; aerospace simulation; aircraft control; control engineering computing; control system synthesis; data visualisation; motion control; nonlinear dynamical systems; Atlas; Flightgear; Matlab; angleof-attack; cobra maneuver simulation; design stage; flight quality requirements; flight simulation; nonlinear dynamic inversion method; normal flight envelope; post-stall maneuverability flight control law design; real time visualization flight simulator; supermaneuverable aircraft; visual simulation research; Aerospace control; Aerospace simulation; Electronic mail; MATLAB; Nonlinear dynamical systems; Visualization; flight control; flight simulation; flightgear; nonlinear dynamic inversion; post-stall maneuverability;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2012 31st Chinese
Conference_Location
Hefei
ISSN
1934-1768
Print_ISBN
978-1-4673-2581-3
Type
conf
Filename
6390000
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