相对失控翻滚目标悬停的自适应模糊滑模控制

doi:10.7527/S1000-6893.2019.22430

Abstract

Abstract: The six degree-of-freedom coupling control of the chaser relative to the uncontrolled tumbling satellite with system uncertainties and external disturbances is studied in this paper. Initially, a non-linear six-degree-of-freedom coupled integrated dynamics model is established in the chaser's body coordinate system, which transforms the hovering control problem into relative position and relative attitude control problems. Then, an adaptive fuzzy sliding mode controller is designed based on the principle of fuzzy approximation. The controller can effectively overcome the uncertainty of the system model and the influence of external disturbance, eliminating the traditional chattering problem. The fuzzy adaptive law is derived from the Lyapunov method and the stability of the closed-loop system is proved. Numerical simulations verify the effectiveness of the proposed adaptive fuzzy sliding mode controller.

Key words: uncontrolled tumbling satellite, hovering control, fuzzy sliding mode control, adaptive control, six degree-of-freedom coupling

CLC Number:

V448.2

LIU Jianghui, LI Haiyang, ZHANG Zheng, LI Xiaochao. Adaptive fuzzy sliding mode control for body-fixed hovering over uncontrolled tumbling satellite[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(5): 322430-322430.

References

[1] 朱战霞, 马家瑨, 樊瑞山. 基于螺旋理论描述的空间相对运动姿轨同步控制[J]. 航空学报, 2016, 37(9):2788-2798. ZHU Z X, MA J J, FAN R S. Synchronization control of relative motion for spacecraft with screw theory-based description[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(9):2788-2798(in Chinese).
[2] 朱亚文, 闫野. 椭圆轨道卫星空间任意位置悬停的方法[J]. 中国空间科学技术, 2010, 30(6):17-23. ZHU Y W, YAN Y. Hovering method at any selected position over space target on elliptical orbit[J]. Chinese Space Science and Technology, 2010, 30(6):17-23(in Chinese).
[3] 周稼康, 胡庆雷, 马广富, 等. 带时变通信时间延迟的卫星编队姿态协同自适应L2增益控制[J]. 航空学报, 2011, 32(2):321-329. ZHOU J K, HU Q L, MA G F, et al. Adaptive L2-gain cooperative attitude control of satellite formation flying with time-varying delay[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(2):321-329(in Chinese).
[4] 王功波, 郑伟, 孟云鹤, 等. 相对非圆轨道的悬停控制方法研究[J]. 中国科学(技术科学), 2011,54(11):1505-1511. WANG G B, ZHENG W, MENG Y H, et al. Research on hovering control scheme to non-circular orbit[J]. Science in China Series E (Technological Sciences), 2011, 54(11):1505-1511(in Chinese).
[5] 王剑颖, 梁海朝, 孙兆伟, 等. 基于对偶数的航天器多特征融合相对导航算法[J]. 航空学报, 2012, 33(10):1881-1892. WANG J Y, LIANG H C, SUN Z W, et al. A multi-cue-based relative navigation algorithm for spacecraft via dual number representation[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(10):1881-1892(in Chinese).
[6] 吴锦杰, 刘昆, 韩大鹏. 考虑输入饱和的航天器相对运动鲁棒自适应控制[J]. 航空学报, 2013, 34(4):890-901. WU J J, LIU K, HAN D P. Robust adaptive control for relative motion of spacecraft under input saturation[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(4):890-901(in Chinese).
[7] SUN L, HUO W, JIAO Z. Robust adaptive relative position and attitude control for spacecraft autonomous proximity[J]. ISA Transactions, 2016, 63:11-19.
[8] BROSCHART S B, SCHEERES D J. Control of hovering spacecraft near small bodies:Application to asteroid 25143 Itokawa[J]. Journal of Guidance Control & Dynamics, 2005, 28(2):343-354.
[9] SCHEERES D J. Stability of hovering orbits around small bodies[J]. Advances in the Astronautical Sciences, 1999, 102:855-875.
[10] SCHEERES D J. Orbital motion in strongly perturbed environments[M]. Berlin:Springer, 2012.
[11] SAWAI S, SCHEERES D J, BROSCHART S B. Control of hovering spacecraft using altimetry[J]. Journal of Guidance Control & Dynamics, 2000, 25(4):786-795.
[12] BROSCHART S B, SCHEERES D J. Boundness of spacecraft hovering under dead-band control in time-invariant systems[J]. Journal of Guidance Control & Dynamics, 2007, 30(2):601-610.
[13] ZENG X, GONG S, LI J, et al. Solar sail body-fixed hovering over elongated asteroids[J]. Journal of Guidance Control & Dynamics, 2016, 39(6):1-9.
[14] BERRY K, SUTTERY B, MAYZ A, et al. OSIRIS-REx Touch-And-Go (TAG) mission design and analysis[C]//36th Annual AAS Guidance and Control Conference, 2013.
[15] GAUDET B, FURFARO R. Robust spacecraft hovering near small bodies in environments with unknown dynamics using reinforcement learning[C]//AIAA/AAS Astrodynamics Specialist Conference. Reston, VA:AIAA, 2012.
[16] KUBOTA T, HASHIMOTO T, UO M, et al. Maneuver strategy for station keeping and global mapping around an asteroid[C]//AIAA/AAS Spaceflight Mechanics. Reston, VA:AIAA, 2001:769-780.
[17] LEE D, SANYAL A K, BUTCHER E A, et al. Almost global asymptotic tracking control for spacecraft body-fixed hovering over an asteroid[J]. Aerospace Science & Technology, 2014, 38(1):105-115.
[18] LEE D, SANYAL A K, BUTCHER E A, et al. Finite-time control for spacecraft body-fixed hovering over an asteroid[J]. IEEE Transactions on Aerospace & Electronic Systems, 2015, 51(1):506-520.
[19] LEE D, SANYAL A K, BUTCHER E A, et al. Spacecraft hovering control for body-fixed hovering over a uniformly rotating asteroid using geometric mechanics[J]. Advances in the Astronautical Sciences, 2014, 150:1757-1773.
[20] 谭天乐, 武海雷. 轨道交会、悬停及绕飞控制的解析解方法[J]. 宇航学报, 2016, 37(11):1333-1341. TAN T L, WU H L. Analytical solution method for orbit rendezvous,hovering and fly-around control[J]. Journal of Astronautics, 2016, 37(11):1333-1341(in Chinese).
[21] 谭天乐. 椭圆轨道交会、悬停与绕飞的全状态反馈控制[J]. 宇航学报, 2016, 37(7):811-818. TAN T L. Full state feedback control of rendezvous,hovering and fly-around in elliptical orbit[J]. Journal of Astronautics, 2016, 37(7):811-818(in Chinese).
[22] 薛白, 佘志坤, 余婧, 等. 基于混杂系统的空间飞行器悬停控制[J]. 中国空间科学技术, 2010, 30(2):61-67. XUE B, SHE Z K, YU J, et al. Control on the spacecraft hovering based on hybrid systems[J]. Chinese Space Science and Technology, 2010, 30(2):61-67(in Chinese).
[23] 程博, 袁建平, 马卫华. 基于状态转移矩阵的航天器多脉冲悬停方法[J]. 中国空间科学技术, 2016, 36(5):81-87. CHENG B, YUAN J P, MA W H. Spacecraft multiple-pulse hovering method based on state transition matrix[J]. Chinese Space Science and Technology, 2016, 36(5):81-87(in Chinese).
[24] 徐帷, 武海雷, 卢山, 等. 航天器超近距离绕飞、悬停的姿态轨道联合控制方法研究[C]//第32届中国控制会议, 2013. XU W, WU H L, LU S, et al. Spacecraft attitude-orbit combined control analysis for flying-around and hovering task in super-close relative distance[C]//the 32nd Chinese Control Conference, 2013(in Chinese).
[25] 宋旭民, 范丽, 陈勇, 等. 相对空间目标任意位置悬停闭环控制方法研究[J]. 中国空间科学技术, 2010, 30(1):41-45. SONG X M, FAN L, CHEN Y, et al. Study of close-loop hovering method at any selected position to space target[J]. Chinese Space Science and Technology, 2010, 30(1):41-45(in Chinese).
[26] DANG Z, WANG Z, ZHANG Y. Modeling and analysis of relative hovering control for spacecraft[J]. Journal of Guidance Control & Dynamics, 2014, 37(4):1091-1102.
[27] SUN L, HUO W. Robust adaptive control of spacecraft proximity maneuvers under dynamic coupling and uncertainty[J]. Advances in Space Research, 2015, 56(10):2206-2217.
[28] SHUSTER M D. A survey of attitude representation[J]. Journal of Astronautical Sciences, 1993, 41(4):439-517.
[29] HAM W. Adaptive fuzzy sliding mode control of nonlinear system[J]. IEEE Transactions on Fuzzy Systems, 1998, 6(2):315-321.

Adaptive fuzzy sliding mode control for body-fixed hovering over uncontrolled tumbling satellite

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Fengying ZHENG, Zhimin SHEN, Yaqin LI, Kaizhao XU, Xinhua WANG. Gain adaptive multi-mode switching control for coaxial high-speed helicopter [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529088-529088.
[2]	Yuqing QIU, Yan LI, Jinxi LANG, Yuxian LIU, Zhong WANG. Robust adaptive attitude control of high-speed helicopters in transition mode [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529927-529927.
[3]	Kai NING, Baolin WU. Event-triggered-based orbit maintenance control for spacecraft subsatellite point control [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(10): 329412-329412.
[4]	Leyan FANG, Han MENG, Mingzhe HOU. Iterative learning sliding mode control with precise parameter estimation and its application [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 628889-628889.
[5]	Guangquan DUAN, Guoping LIU. Adaptive prescribed control of position and attitude of combined spacecraft based on fully actuated system approach [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 628837-628837.
[6]	Xiaoyun SUN, Shufan WU, Qiang SHEN. LMI-based output tracking robust drag-free control with model reference adaptive scheme [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S1): 727654-727654.
[7]	Runchang HU, Zian WANG, Yongliang CHEN, Dapeng ZHOU, Dapeng YANG, Zheng GONG. Stability augmentation control of thrust-vectored V/STOL aircraft based on L1 adaptive control [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S1): 727642-727642.
[8]	Chenyang LIU, Dawei WU, Yize GUO, Xinsai LV, Jiani ZHOU, Shuyi SHAO. Robust adaptive attitude control of quadrotor with uncertain strong coupling [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S1): 727645-727645.
[9]	Yajie MA, Juan WANG, Bin JIANG, Jianye GONG. A fault⁃tolerant control scheme for UAVs-UGVs formation systems [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(8): 327216-327216.
[10]	Feiyan GUO, Jianhua LIU, Qingdong XIAO, Shihong XIAO, Zhongqi WANG. Monitoring and evaluation of working condition and adaptive control technology for digital assembly tooling [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(16): 427914-427914.
[11]	YANG Xiaowei, GE Yaowen, DENG Wenxiang, YAO Jianyong, ZHOU Ning. Active fault-tolerant control for hydraulic actuating cylinders of aeroengine guide vane control mechanisms [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(9): 625464-625464.
[12]	WU Baohai, ZHANG Yang, ZHENG Zhiyang, ZHANG Ying, ZHANG Siqi. Review and prospects of feedrate optimization in CNC machining [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(4): 525467-525467.
[13]	SHI Zhongjiao, ZHU Huajie, ZHAO Liangyu, LIU Zhijie. Adaptive decoupling control for a class of spinning rockets considering actuator dynamics [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(3): 325068-325068.
[14]	ZHANG Pu, XUE Huifeng, GAO Shan. Distributed adaptive fault-tolerance consensus control for multi-agent system [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(3): 323539-323539.
[15]	ZHANG Jialong, YAN Jianguo, ZHANG Pu. Multi-UAV formation forming control based on adaptive method under wind field disturbances [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(1): 323385-323385.