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2012 (Vol. 4, Issue: 18)
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 

Key words:  Adaptive, missile, robustness, sliding mode, supersonic, ,
Vol. 4 , (18): 3488-3492
Submitted Accepted Published
April 25, 2012 May 13, 2012 September 15, 2012

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.
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  Cite this Reference:
Gangling Jiao, Yuqiang Jin and Shixing Wang, 2012. Research on the Robustness of an Adaptive PID Control of a Kind of Supersonic Missile.  Research Journal of Applied Sciences, Engineering and Technology, 4(18): 3488-3492.
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ISSN (Online):  2040-7467
ISSN (Print):   2040-7459
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