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Proceedings Paper

Robust control for snake maneuver design of missile
Author(s): Ya Kun; Xin Chen; Chuntao Li
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Paper 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.

Paper Details

Date Published: 23 January 2017
PDF: 10 pages
Proc. SPIE 10322, Seventh International Conference on Electronics and Information Engineering, 103223H (23 January 2017); doi: 10.1117/12.2265316
Show Author Affiliations
Ya Kun, Nanjing Univ. of Aeronautics and Astronautics (China)
Xin Chen, Nanjing Univ. of Aeronautics and Astronautics (China)
Chuntao Li, Nanjing Univ. of Aeronautics and Astronautics (China)


Published in SPIE Proceedings Vol. 10322:
Seventh International Conference on Electronics and Information Engineering
Xiyuan Chen, Editor(s)

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