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Attitude tracking control for Mars entry vehicle via T-S model with time-varying input delay

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Abstract

This paper focuses on the attitude tracking control problem of Mars entry vehicle (MEV) with time-varying input delay. The original attitude dynamics of MEV is divided into slow subsystem and fast subsystem. For slow subsystem, the dynamic inversion method is used to generate the angular velocity command. For fast subsystem, a T-S fuzzy model is used to approximate it, and delays-dependent \(H_{\infty }\) attitude tracking control is applied to reduce the effects of delay on attitude dynamics. Specially, a decomposition coefficient of delay integral inequality is introduced in our proposed results, which may further reduce the design algorithm conservatism. Finally, numerical simulations are used to verify the effectiveness of the proposed method.

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Acknowledgments

This work is supported by National Nature Science Foundation under Grant: 61573189, 61573190; Nature Science Foundation of Jiangsu Province: BK20140045, BK20131000, BK20150927; and Six talent peaks project in Jiangsu Province: 2015-DZXX-013.

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Authors and Affiliations

  1. School of Instrumentation Science and Opto-Electronics Engineering, Beihang University, Beijing, 100191, China

    Furong Lei

  2. B-DAT, CICAEET, School of Information and Control, Nanjing University of Information Science and Technology, Nanjing, 210044, China

    Xiaofeng Xu, Tao Li & Gongfei Song

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  1. Furong Lei
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  2. Xiaofeng Xu
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  3. Tao Li
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  4. Gongfei Song
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Correspondence to Tao Li.

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Lei, F., Xu, X., Li, T. et al. Attitude tracking control for Mars entry vehicle via T-S model with time-varying input delay. Nonlinear Dyn 85, 1749–1764 (2016). https://doi.org/10.1007/s11071-016-2791-4

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  • DOI: https://doi.org/10.1007/s11071-016-2791-4

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