Research on Robustness of Double PID Control of Supersonic Missiles
作者： Wenguang Zhang , Junwei Lei , Xianjun Shi , Guoqiang Liang , None
DOI: 10.1007/978-3-642-27452-7_80
关键词:
摘要: Based on the multi-loop design method, dynamic characteristic of missile system is viewed as a two loops such inner loop and outer loop. A double PID control strategy designed for pitch channel linear model supersonic missile. The robustness controller analyzed by changing air-dynamic coefficients. And law testified to be stable even air coefficients changed 0.7 1.7 times its standard value.
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