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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: Zhixiang Hou
Submitted: December 20, 2011
Accepted: July 18, 2012
Published: January 01, 2013 |
Abstract:
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In this study, the dynamic characteristic of missile system is viewed as a two-loop system, such as inner
loop and outer loop and we design an adaptive PID control strategy 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, (01): 37-41.
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ISSN (Online): 2040-7467
ISSN (Print): 2040-7459 |
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