空间非合作航天器抓捕后姿态抗干扰控制

doi:10.7527/S1000-6893.2020.24849

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空间非合作航天器抓捕后姿态抗干扰控制

刘闯^1,2, 岳晓奎^1,2

1. 西北工业大学航天学院, 西安 710072;
2. 西北工业大学航天飞行动力学技术重点实验室, 西安 710072

收稿日期:2020-10-09 修回日期:2020-12-20 发布日期:2021-01-14
通讯作者: 岳晓奎 E-mail:xkyue@nwpu.edu.cn
基金资助:
国家自然科学基金（62103336，11972026，U2013206）；陕西省自然科学基金（2020JQ-132）；中国博士后科学基金（2020M683571）；陕西省科协青年人才托举计划（2021-1-2）；国防科技重点实验室基金（6142210200310）；中央高校基本科研业务费专项资金（3102019HTQD007）

Anti-disturbance attitude control for post-capture non-cooperative spacecraft

LIU Chuang^1,2, YUE Xiaokui^1,2

1. School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China;
2. National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University, Xi'an 710072, China

Received:2020-10-09 Revised:2020-12-20 Published:2021-01-14
Supported by:
National Natural Science Foundation of China (62103336, 11972026, U2013206); Natural Science Foundation of Shaanxi Province (2020JQ-132); China Postdoctoral Science Foundation (2020M683571); Young Talent Fund of Shaanxi Association for Science and Technology (2021-1-2); the Science and Technology Foundation of National Key Laboratory of Aerospace Flight Dynamics (6142210200310); the Fundamental Research Funds for the Central Universities (3102019HTQD007)

摘要/Abstract

摘要： 针对空间非合作航天器抓捕后存在未知不确定惯性参数的柔性组合体姿态稳定控制问题，基于中间状态观测器设计方法提出了一种新的姿态稳定抗干扰控制方法，同时考虑了诸多扰动及控制输入受限问题。研究结果表明，传统的姿态稳定控制方法需要已知柔性航天器惯性参数信息及状态信息，上述信息未知情况下会使姿态难以高精度稳定控制，且容易导致控制输入不满足受限要求。针对该问题，考虑控制输入幅值及变化率受限前提，提出了一种基于中间状态观测器的抗干扰控制方法，通过引入辅助变量构造新型中间状态观测器，同时估计组合体状态信息及综合干扰，设计出了一种新的组合体姿态稳定抗干扰控制器。通过Lyapunov稳定性分析方法证明了所设计的控制器能够保证闭环系统的全局渐近稳定性。相比于已有的混合H₂/H_∞控制器，所提出的抗干扰控制器在应用时不需要柔性组合体的姿态及模态信息，并且也不需要惯性参数的辨识过程。最后，通过给定参数进行仿真对比，进一步验证了所设计控制器的有效性和优越性。

关键词: 非合作航天器, 空间抓捕后, 姿态控制, 抗干扰控制, 振动抑制

Abstract: For the attitude stabilization control problem of post-capture non-cooperative spacecraft with unknown and uncertain inertial parameters, a novel anti-disturbance attitude control method is proposed based on an intermediate state observer, while considering multiple disturbances and control input magnitude and rate constraints. The traditional attitude stabilization control methods often need known information on the inertial parameter and state of the flexible spacecraft. If the above information is unknown, it will be difficult to achieve attitude stabilization with high precision, and it will be easy to cause the control input to be not able to meet the restricted requirements. To solve this problem, considering the control input magnitude and rate constraints, an anti-disturbance control method is proposed based on an intermediate state observer. The observer is constructed by introducing an auxiliary variable using the state information and lump disturbance, and a novel anti-disturbance controller is then designed. The Lyapunov stability analysis method is used to prove that the designed controller can ensure the global asymptotic stability of the closed-loop system. Compared with the existing mixed H₂/H_∞ controller, the developed controller does not require the attitude and modal information of the flexible body, and the identification process of inertial parameters either. Finally, simulation comparisons further verify the effectiveness and superiority of the designed controller.

Key words: non-cooperative spacecraft, space post-capture, attitude control, anti-disturbance control, vibration suppression

中图分类号:

V448.2

刘闯, 岳晓奎. 空间非合作航天器抓捕后姿态抗干扰控制[J]. 航空学报, 2021, 42(11): 524849-524849.

LIU Chuang, YUE Xiaokui. Anti-disturbance attitude control for post-capture non-cooperative spacecraft[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(11): 524849-524849.

参考文献

[1] SUN L, ZHENG Z W. Disturbance-observer-based robust backstepping attitude stabilization of spacecraft under input saturation and measurement uncertainty[J]. IEEE Transactions on Industrial Electronics, 2017, 64(10):7994-8002.
[2] 陈雪芹, 孙瑞, 吴凡, 等. 基于ATSUKF算法的卫星姿控系统故障估计[J]. 航空学报, 2019, 40(5):322551. CHEN X Q, SUN R, WU F, et al. Fault estimation in satellite attitude control system based on ATSUKF algorithm[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(5):322551(in Chinese).
[3] HU Q L, SHAO X D, CHEN W H. Robust fault-tolerant tracking control for spacecraft proximity operations using time-varying sliding mode[J]. IEEE Transactions on Aerospace and Electronic Systems, 2018, 54(1):2-17.
[4] SINGH S N, ZHANG R. Adaptive output feedback control of spacecraft with flexible appendages by modeling error compensation[J]. Acta Astronautica, 2004, 54(4):229-243.
[5] LEE K W, SINGH S N. L₁ adaptive control of flexible spacecraft despite disturbances[J]. Acta Astronautica, 2012, 80:24-35.
[6] ZHENG J H, BANKS S P, ALLEYNE H. Optimal attitude control for three-axis stabilized flexible spacecraft[J]. Acta Astronautica, 2005, 56(5):519-528.
[7] LIU C, YE D, SHI K K, et al. Robust high-precision attitude control for flexible spacecraft with improved mixed H₂/H_∞ control strategy under poles assignment constraint[J]. Acta Astronautica, 2017, 136:166-175.
[8] 张秀云, 宗群, 窦立谦, 等. 柔性航天器振动主动抑制及姿态控制[J]. 航空学报, 2019, 40(4):322503. ZHANG X Y, ZONG Q, DOU L Q, et al. Active vibration suppression and attitude control for flexible spacecraft[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(4):322503(in Chinese).
[9] HU Q L. Robust adaptive sliding-mode fault-tolerant control with L₂-gain performance for flexible spacecraft using redundant reaction wheels[J]. IET Control Theory & Applications, 2010, 4(6):1055-1070.
[10] MA Y J, JIANG B, TAO G, et al. Uncertainty decomposition-based fault-tolerant adaptive control of flexible spacecraft[J]. IEEE Transactions on Aerospace and Electronic Systems, 2015, 51(2):1053-1068.
[11] YAN R D, WU Z. Attitude stabilization of flexible spacecrafts via extended disturbance observer based controller[J]. Acta Astronautica, 2017, 133:73-80.
[12] WU S N, WEN S H. Robust H_∞ output feedback control for attitude stabilization of a flexible spacecraft[J]. Nonlinear Dynamics, 2016, 84(1):405-412.
[13] WEISS A, KOLMANOVSKY I, BERNSTEIN D S, et al. Inertia-free spacecraft attitude control using reaction wheels[J]. Journal of Guidance, Control, and Dynamics, 2013, 36(5):1425-1439.
[14] SANYAL A, FOSBURY A, CHATURVEDI N, et al. Inertia-free spacecraft attitude tracking with disturbance rejection and almost global stabilization[J]. Journal of Guidance, Control, and Dynamics, 2009, 32(4):1167-1178.
[15] SONG G B, AGRAWAL B N. Vibration suppression of flexible spacecraft during attitude control[J]. Acta Astronautica, 2001, 49(2):73-83.
[16] DI GENNARO S. Output stabilization of flexible spacecraft with active vibration suppression[J]. IEEE Transactions on Aerospace and Electronic Systems, 2003, 39(3):747-759.
[17] MOON S H, CHWA D, KIM S J. Feedback linearization control for panel flutter suppression with piezoelectric actuators[J]. AIAA Journal, 2005, 43(9):2069-2073.
[18] HU Q L, SHAO X D, ZHANG Y M, et al. Nussbaum-type function-based attitude control of spacecraft with actuator saturation[J]. International Journal of Robust and Nonlinear Control, 2018, 28(8):2927-2949.
[19] SU Y X, ZHENG C H. Globally asymptotic stabilization of spacecraft with simple saturated proportional-derivative control[J]. Journal of Guidance, Control, and Dynamics, 2011, 34(6):1932-1936.
[20] HU Q L, SHI Y X, SHAO X D. Adaptive fault-tolerant attitude control for satellite reorientation under input saturation[J]. Aerospace Science and Technology, 2018, 78:171-182.
[21] GUO Y, HUANG B, GUO J H, et al. Velocity-free sliding mode control for spacecraft with input saturation[J]. Acta Astronautica, 2019, 154:1-8.
[22] XIAO B, YIN S, KAYNAK O. Attitude stabilization control of flexible satellites with high accuracy:An estimator-based approach[J]. IEEE/ASME Transactions on Mechatronics, 2017, 22(1):349-358.
[23] ZHONG C X, CHEN Z Y, GUO Y. Attitude control for flexible spacecraft with disturbance rejection[J]. IEEE Transactions on Aerospace and Electronic Systems, 2017, 53(1):101-110.
[24] WANG H M, YANG G H. Robust mixed l₁/H_∞ filtering for affine fuzzy systems with measurement errors[J]. IEEE Transactions on Cybernetics, 2014, 44(7):1100-1110.
[25] LIU C, SHI K K, YUE X K, et al. Inertia-free saturated output feedback attitude stabilization for uncertain spacecraft[J]. International Journal of Robust and Nonlinear Control, 2020, 30(13):5101-5121.
[26] GE S S, WANG C. Adaptive neural control of uncertain MIMO nonlinear systems[J]. IEEE Transactions on Neural Networks, 2004, 15(3):674-692.
[27] YANG C D, SUN Y P. Mixed H₂/H_∞ state-feedback design for microsatellite attitude control[J]. Control Engineering Practice, 2002, 10(9):951-970.
[28] LIU C, VUKOVICH G, SUN Z W, et al. Observer-based fault-tolerant attitude control for spacecraft with input delay[J]. Journal of Guidance, Control, and Dynamics, 2018, 41(9):2041-2053.
[29] SHI K K, LIU C, BIGGS J D, et al. Observer-based control for spacecraft electromagnetic docking[J]. Aerospace Science and Technology, 2020, 99:105759.
[30] LIU C, SHI K K, SUN Z W. Robust H_∞ controller design for attitude stabilization of flexible spacecraft with input constraints[J]. Advances in Space Research, 2019, 63(5):1498-1522.

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空间非合作航天器抓捕后姿态抗干扰控制

Anti-disturbance attitude control for post-capture non-cooperative spacecraft

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