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Volume 7 Issue 2
Mar.  2020

IEEE/CAA Journal of Automatica Sinica

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Article Navigation >  IEEE/CAA Journal of Automatica Sinica  > 2020  >  7(2): 472-481
Yun Li and Fan Yang, "Robust Adaptive Attitude Control for Non-rigid Spacecraft With Quantized Control Input," IEEE/CAA J. Autom. Sinica, vol. 7, no. 2, pp. 472-481, Mar. 2020. doi: 10.1109/JAS.2020.1003000
Citation: Yun Li and Fan Yang, "Robust Adaptive Attitude Control for Non-rigid Spacecraft With Quantized Control Input," IEEE/CAA J. Autom. Sinica, vol. 7, no. 2, pp. 472-481, Mar. 2020. doi: 10.1109/JAS.2020.1003000
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Robust Adaptive Attitude Control for Non-rigid Spacecraft With Quantized Control Input

doi: 10.1109/JAS.2020.1003000
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    Abstract
  • In this paper, an adaptive backstepping control scheme is proposed for attitude tracking of non-rigid spacecraft in the presence of input quantization, inertial uncertainty and external disturbance. The control signal for each actuator is quantized by sector-bounded quantizers, including the logarithmic quantizer and the hysteresis quantizer. By describing the impact of quantization in a new affine model and introducing a smooth function and a novel form of the control signal, the influence caused by input quantization and external disturbance is properly compensated for. Moreover, with the aid of the adaptive control technique, our approach can achieve attitude tracking without the explicit knowledge of inertial parameters. Unlike existing attitude control schemes for spacecraft, in this paper, the quantization parameters can be unknown, and the bounds of inertial parameters and disturbance are also not needed. In addition to proving the stability of the closed-loop system, the relationship between the control performance and design parameters is analyzed. Simulation results are presented to illustrate the effectiveness of the proposed scheme.

     

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  • [1]
    O. Brown, P. Eremenko, and C. Roberts, “Cost-benefit analysis of a notional fractionated SATCOM architecture,” in Proc. 24th AIAA Int. Communication Satellite Systems Conf., CA, USA, AIAA 2006–5328, 2006.
    [2]
    O. Brown and P. Eremenko, “The value proposition for fractionated space architectures,” in Proc. AIAA Space Forum, CA, USA, AIAA 2006–7506, 2006.
    [3]
    D. Fronterhouse, J. Lyke, and S. Achramowicz, “Plug-and-play satellite (PnPSat),” in Proc. AIAA Infotech Aerospace Conf. and Exhibit, CA, USA, AIAA 2007–2914, 2007.
    [4]
    J. Lyke, “Plug-and-play satellites,” IEEE Spectrum, vol. 49, no. 8, pp. 36–42, 2012. doi: 10.1109/MSPEC.2012.6247560
    [5]
    H. Ishii and B. Francis, Limited Data Rate in Control Systems With Networks. Springer Berlin Heidelberg, 2002.
    [6]
    S. Tatikonda and S. Mitter, “Control under communication constraints,” IEEE Trans. Automatic Control, vol. 49, no. 7, pp. 1056–1068, 2004. doi: 10.1109/TAC.2004.831187
    [7]
    J. Zhou, C. Y. Wen, and G. H. Yang, “Adaptive backstepping stabilization of nonlinear uncertain systems with quantized input signal,” IEEE Trans. Autom. Control, vol. 59, no. 2, pp. 460–464, 2014. doi: 10.1109/TAC.2013.2270870
    [8]
    R. Sharma and A. Tewari, “Optimal nonlinear tracking of spacecraft attitude maneuvers,” IEEE Trans. Control Systems Technology, vol. 12, no. 5, pp. 677–682, 2013.
    [9]
    B. L. Wu, D. W. Wang, and E. K. Poh, “High precision satellite attitude tracking control via iterative learning control,” J. Guidance Control &Dynamics, vol. 38, no. 3, pp. 528–534, 2015.
    [10]
    H. P. Li, W. S. Yan, and Y. Shi, “Continuous-time model predictive control of under-actuated spacecraft with bounded control torques,” Automatica, vol. 75, pp. 144–153, 2017. doi: 10.1016/j.automatica.2016.09.024
    [11]
    S. N. Wu and S. H. Wen, “Robust H∞ output feedback control for attitude stabilization of a flexible spacecraft,” Nonlinear Dynamics, vol. 84, pp. 405–412, 2016. doi: 10.1007/s11071-016-2624-5
    [12]
    S. C. Liu, Z. Y. Geng, and J. Y. Sun, “Finite-time attitude control: a finite-time passivity approach,” IEEE/CAA J Autom. Sinica, vol. 2, no. 1, pp. 102–108, 2015. doi: 10.1109/JAS.2015.7032911
    [13]
    W. C. Cai, X. H. Liao, and Y. D. Song, “Indirect robust adaptive fault -tolerant control for attitude tracking of spacecraft,” J. Guidance Control &Dynamics, vol. 31, no. 5, pp. 1456–1463, 2008.
    [14]
    W. C. Luo, Y. C. Chu, and K. V. Ling, “Inverse optimal adaptive control for attitude tracking of spacecraft,” IEEE Trans. Autom. Control, vol. 50, no. 11, pp. 1639–1654, 2005. doi: 10.1109/TAC.2005.858694
    [15]
    D. Seo and M. Akella, “High-performance spacecraft adaptive attitudetracking control through attracting-manifold design,” J. Guidance Control &Dynamics, vol. 31, no. 4, pp. 884–891, 2008.
    [16]
    Q. L. Hu, X. D. Shao, and L. Guo, “Adaptive fault-tolerant attitude tracking control of spacecraft with prescribed performance,” IEEE/ASME Trans. Mechatronics, vol. 23, no. 1, pp. 331–341, 2018. doi: 10.1109/TMECH.2017.2775626
    [17]
    D. Thakur, S. Srikant, and M. Akella, “Adaptive attitude-tracking control of spacecraft with uncertain time-varying inertia parameters,” J. Guidance Control &Dynamics, vol. 38, no. 1, pp. 41–52, 2015.
    [18]
    Q. L. Hu, Y. X. Shi, and X. D. Shao, “Adaptive fault-tolerant attitude control for satellite reorientation under input saturation,” Aerospace Science &Technology, vol. 78, pp. 171–182, 2018.
    [19]
    Y. Li, C. L. Wang, and W. Wang. Adaptive quantized attitude control for spacecraft with input saturation. in Proc. IEEE Int. Conf. Control & Automation, Ohrid, Macedonia, 449–454, 2017.
    [20]
    B. L. Wu, “Spacecraft attutude control with input quantization,” J. Guidance Control &Dynamics, vol. 39, no. 1, pp. 176–181, 2015.
    [21]
    X. Y. Lang, J. Damaren, and X. B. Cao, “Passivity-based attitude control with input quantization,” Institution of Mechanical Engineering Part G: J. Aerospace Engineering, 2018.
    [22]
    H. B. Sun, L. L. Hou, G. D. Zong, and X. H. Yu, “Fixed-time attitude tracking control for spacecraft with input quantization,” IEEE Trans. Aerospace &Electronic Systems, vol. 55, no. 1, pp. 124–134, 2019.
    [23]
    B. L. Wu and X. B. Cao, “Robust attitude tracking control for spacecraft with quantized torques,” IEEE Trans. Aerospace &Electronic Systems, vol. 54, no. 2, pp. 1020–1028, 2018.
    [24]
    C. L. Wang and Y. Lin, “Decentralized adaptive tracking control for a class of interconnected nonlinear time-varying systems,” Automatica, vol. 54, pp. 16–24, 2015. doi: 10.1016/j.automatica.2015.01.041
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    Highlights

    • An adaptive control scheme is proposed for attitude tracking of spacecraft.
    • Input quantization is properly dealt with by a bound estimation approach.
    • Attitude control is achieved in the presence of time-varying inertial parameters.
    • The relationship of control performance and quantization parameters is analyzed.

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