2013
DOI: 10.19026/rjaset.5.5081
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Research on the Robustness of an Adaptive PID Control of a Kind of Supersonic Missile

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 … Show more

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“…Jiao, Jin and Wang (2013) analyzed the robustness of a double PID controller for a missile system by changing the aerodynamic coefficients. They viewed the dynamic characteristics as a two-loop system and designed an adaptive PID control strategy for the pitch channel linear model of supersonic missile [14]. studied the robustness of a number of controllers and compensators from the second generation of PID-based controllers and lag-lead compensators [15][16][17].…”
Section: Introductionmentioning
confidence: 99%
“…Jiao, Jin and Wang (2013) analyzed the robustness of a double PID controller for a missile system by changing the aerodynamic coefficients. They viewed the dynamic characteristics as a two-loop system and designed an adaptive PID control strategy for the pitch channel linear model of supersonic missile [14]. studied the robustness of a number of controllers and compensators from the second generation of PID-based controllers and lag-lead compensators [15][16][17].…”
Section: Introductionmentioning
confidence: 99%