Disturbance compensated terminal sliding mode control for hypersonic vehicles

Zeng Xianfa; Wang Xiaohu; Zhang Jing; Shen Gongzhang

Volume 38 Issue 11

Nov. 2012

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Journal of Beijing University of Aeronautics and Astronautics > 2012 > (11): 1454-1458.

Zhu Kuibao, Zhang Chunxi, Song Ningfanget al. Modeling and identification of random drift for FOG[J]. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(11): 1354-1357. (in Chinese)

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Zeng Xianfa, Wang Xiaohu, Zhang Jing, et al. Disturbance compensated terminal sliding mode control for hypersonic vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (11): 1454-1458. (in Chinese)

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Disturbance compensated terminal sliding mode control for hypersonic vehicles

1.
Beijing Institute of Control & Electronics Technology, Beijing 100038, China
2. School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

Received Date: 17 Jun 2011
Publish Date: 30 Nov 2012

Abstract

Abstract

An attitude control approach for hypersonic vehicles based on disturbance compensated terminal sliding mode(TSM) was studied. First, a modified TSM surface which switched to high gain linear sliding mode surface while in the neighborhood of equilibrium point was proposed to overcome the singularity problem of traditional TSM, and maintain the high rate of convergence. Then the error convergence property of the proposed TSM in the presence of disturbances was analyzed theoretically. To improve the robustness and precision of TSM control, extended state observer(ESO) was designed to estimate and compensate for disturbances. Finally, 6-degree of freedom numerical simulation was carried out, and the simulation results demonstrate that the control performance and robustness are improved by the proposed method.
- attitude control,
- terminal sliding mode,
- extended state observer,
- disturbance estimation,
- adaptive control

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References(9)

References

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Disturbance compensated terminal sliding mode control for hypersonic vehicles