Sliding Mode Auto - Disturbance Rejection Control of Hypersonic Vehicle under Disturbance

doi:10.16182/j.issn1004731x.joss.201710021

Abstract

Abstract: The strong coupling of the hypersonic vehicle, the high order of the model, and the perturbation of the aerodynamic parameters make it difficult for the general controller to achieve the desired control effect. The self-disturbing tandem technique can well meet the requirements of the high-order model control. The use of sliding mode variable structure technology which is not sensitive to perturbation of parameters can enhance the system immunity. The simulation results show that the control effect is very good.

Key words: High-flying aircraft, auto-disturbance-rejection control, series control, sliding mode variable structure control

CLC Number:

TP391.9

Cheng Mingzhi, Wu Yunjie, Ma Fei. Sliding Mode Auto - Disturbance Rejection Control of Hypersonic Vehicle under Disturbance[J]. Journal of System Simulation, 2017, 29(10): 2391-2397.

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