DocumentCode :
489694
Title :
Control of a High Performance Aircraft with Unacceptable Zerodynamics
Author :
Gopalswamy, Swaminathan ; Hedrick, J. Karl
fYear :
1992
fDate :
24-26 June 1992
Firstpage :
1834
Lastpage :
1838
Abstract :
Nonlinear control techniques such as sliding control cannot be directly applied to control the dynamics of many high performance aircraft such as the AFTI-FI6, as they exhibit unacceptable zerodynamics. Traditionally, approximations have been resorted to, to overcome this problem. In this paper, we apply an "output redefinition" technique to systematically overcome the serodynamics problem, resulting in precise, local, tracking. Computer simulations of high g-commands illustrate that while acceptable tracking can be achieved through the output-redefinition technique, standard nonlinear techniques fail.
Keywords :
Actuators; Aerodynamics; Aerospace control; Aerospace engineering; Aircraft propulsion; Computer simulation; Control systems; High performance computing; Nonlinear control systems; Sliding mode control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1992
Conference_Location :
Chicago, IL, USA
Print_ISBN :
0-7803-0210-9
Type :
conf
Filename :
4792429
Link To Document :
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