23 January 2017 Robust control for snake maneuver design of missile
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Proceedings Volume 10322, Seventh International Conference on Electronics and Information Engineering; 103223H (2017) https://doi.org/10.1117/12.2265316
Event: Seventh International Conference on Electronics and Information Engineering, 2016, Nanjing, China
Abstract
For the performance of missile with high Mach number and strongly nonlinear dynamics, this paper uses robust control to design maneuver controller. Robust servomechanism linear quadratic regulator (RSLQR) control is used to form the inner loop and proportional-plus-integral (PI) control is used to provide yawing tracking with no error. Contrast simulations under three types of deviation have been done to confirm robustness of the RSLQR-plus-PI control. Simulation results shows that RSLQR-plus-PI control would resist the disturbance and maintain the properties of the controller, guarantee the robustness and stability of missile more effectively than pure PI control.
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Ya Kun, Ya Kun, Xin Chen, Xin Chen, Chuntao Li, Chuntao Li, } "Robust control for snake maneuver design of missile", Proc. SPIE 10322, Seventh International Conference on Electronics and Information Engineering, 103223H (23 January 2017); doi: 10.1117/12.2265316; https://doi.org/10.1117/12.2265316
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