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Abstract
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Article Information:
Research on the Robustness of an Adaptive PID Control of a Kind of Supersonic Missile
Gangling Jiao, Yuqiang Jin and Shixing Wang
Corresponding Author: Gangling Jioa
Submitted: April 25, 2012
Accepted: May 13, 2012
Published: September 15, 2012 |
Abstract:
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Based on the multi-loop design method, the dynamic characteristic of missile system is viewed as
a two-loops system, such as inner loop and outer loop. An adaptive PID control strategy is designed for the
pitch channel linear model of supersonic missile. The robustness of a double PID controller is analyzed by
changing the aerodynamic coefficients. The control law is testified to be stable even the aerodynamic
coefficients are changed between 0.7 and 1.7 times of its standard value and the control effect is compared with
the sliding mode control strategy. Also the advantage and defect of both control strategy are summarized at the
end of this study.
Key words: Adaptive, missile, robustness, sliding mode, supersonic, ,
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Abstract
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Cite this Reference:
Gangling Jiao, Yuqiang Jin and Shixing Wang, . Research on the Robustness of an Adaptive PID Control of a Kind of Supersonic Missile. Research Journal of Applied Sciences, Engineering and Technology, (18): 3488-3492.
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ISSN (Online): 2040-7467
ISSN (Print): 2040-7459 |
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