Sliding Mode Observer and Controller Design for Nonlinear Supersonic Missile

Hong Chao Zhao; Xian Jun Shi; Ting Wang

doi:10.4028/www.scientific.net/AMR.718-720.1228

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 718-720Sliding Mode Observer and Controller Design for...

Sliding Mode Observer and Controller Design for Nonlinear Supersonic Missile

Abstract:

The nonlinear equations of motion were constructed for a supersonic anti-warship missile. In order to estimate the unknown angle-of-attack, a sliding mode observer was designed. The convergence capability of the sliding mode observer was analyzed according to the Lyapunov stability theory. A sliding mode controller was designed to drive the missile normal overload output to track its command, based on the output-redefinition approach. In order to confirm the performance of the designed sliding mode observer and controller, a simulation example was carried out for nonlinear missile model. The simulation results show the fast convergence capability of the designed sliding mode observer and controller.

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Periodical:

Advanced Materials Research (Volumes 718-720)

Pages:

1228-1233

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.718-720.1228

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Online since:

July 2013

Authors:

Hong Chao Zhao, Xian Jun Shi, Ting Wang

Keywords:

Normal Overload, Output-Redefinition, Sliding Mode Observer (SMO), Supersonic Anti-Warship Missile

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