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2013 (Vol. 5, Issue: 01)
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 

Key words:  Adaptive, missile, robustness, sliding mode, supersonic, ,
Vol. 5 , (01): 37-41
Submitted Accepted Published
December 20, 2011 July 18, 2012 January 01, 2013
Abstract:

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.
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  Cite this Reference:
Gangling Jiao, Yuqiang Jin and Shixing Wang, 2013. Research on the Robustness of an Adaptive PID Control of a Kind of Supersonic Missile.  Research Journal of Applied Sciences, Engineering and Technology, 5(01): 37-41.
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ISSN (Online):  2040-7467
ISSN (Print):   2040-7459
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