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
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