欠驱动航天器滑模速率阻尼控制

doi:10.3969/j.issn.1674-1579.2013.04.003

Abstract

Abstract: A sliding mode rate damping controller is designed for underactuated spacecraft with one of the three axes actuators invalid. The stabilization problem of the system is addressed, and the disturbance rejection performance is analyzed. The guideline of tuning parameters for the controller is presented. By regarding product of inertia as external disturbance, the problem of designing a controller for underactuated spacecraft with non-diagonal inertia matrix is resolved. The application aspects are considered, such as the switching feature of thrusters, the saturation characteristics of rate gyroscope, the existence of external disturbance and the non-diagonal property of the inertia matrix. Numerical simulation results demonstrate the effectiveness and practicability of the designed controller.

Key words: underactuated spacecraft, sliding mode control, rate damping, thrusters

CLC Number:

GUO Chaoli, ZHANG Duzhou, WANG Shuyi. Sliding Mode Control for Rate Damping of Underactuated Spacecraft[J]., 2013, 39(4): 12-17.

0
/ / Recommend

Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks

URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2013.04.003

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2013/V39/I4/12

References

1］Crouch P E. Spacecraft attitude control and stabilization：applications of geometric control theory to rigid body models［J］. IEEE Transactions on Automatic Control, 1984, 29(4): 321-331 ［2］Krishnan H, McClamroch H, Reyhanoglu M. On the attitude stabilization of a rigid spacecraft using two control torques［C］. American Control Conference, Chicago, USA, 1992 ［3］Wang D X, Jia Y H, Jin L. Controllability of an underactuated spacecraft with one thruster under disturbance［J］. Acta Mechanica Sinica, 2012, 28(3): 838-847 ［4］Victoria C C. Detumbling and reorienting underactuated rigid spacecraft［J］. Journal of Guidance Control and Dynamics, 1996, 19(3):708-710 ［5］张兵，吴宏鑫. 非完整配置下姿态翻滚抑制的滑动控制［J］. 宇航学报, 2000, 21(2):35-42 Zhang B, Wu H X. Sliding mode control for attitude detumbling under incomplete configuration［J］. Journal of Astronautics, 2000,21(2):35-42 ［6］Eshaghi R, Paul K C W , Fred Y H. A Lyapunovbased failsafe controller for an underactuated rigidbody spacecraft［C］. AIAA Guidance, Navigation and Control Conference, Montreal, Canada, 2001 ［7］Behal A, Dawson D, Zergeroglu E, et al. Nonlinear tracking control of an underactuated spacecraft［J］. Journal of Guidance Control and Dynamics, 2002, 25(5): 979-985 ［8］林壮,段广仁. 欠驱动刚体航天器姿态机动滑模控制研究［J］. 控制与决策, 2010, 25(3): 389393 Lin Z , Duan G R. Research on sliding mode control for underactuated rigid spacecraft attitude maneuver［J］. Control and Decision, 2010, 25(3): 389-393 ［9］Aeyeles D .Stabilization of a class of nonlinear systems by a smooth feedback control［J］. Systems and Control Letters, 1985, 6(1): 289-294 ［10］高为炳. 变结构控制的理论及设计方法［M］. 北京：科学出版社, 1996

[1]	LI Jiahui, HAN Yajie, LI Yong, XIA Guangqing, LIU Xuhui, SUN Anbang, SUN Bin, HAN Daoman, LU Chang. Progress of RF Ion Thruster [J]. Aerospace Contrd and Application, 2021, 47(4): 21-30.
[2]	ZHANG Wenhui, CHEN Haowen, WEN Zhi, YE Xiaoping. Sliding Mode Control of Flexible Joint Space Robot for Unknown Target [J]. Aerospace Contrd and Application, 2021, 47(3): 49-56.
[3]	DENG Ruchuan, ZHAO Di, ZHANG Shan, GOU Hao, FU Jianhao, ZHENG Liang, FEI Ling. Performance Analysis of the Combined Speed Sliding Mode and Current Prediction Controller of Permanent Magnet Synchronous Motor [J]. Aerospace Contrd and Application, 2021, 47(3): 64-72.
[4]	HE Jingjiu, YUAN Changqing, ZUO Chenyi. Formation Keeping Control of Hybrid Propulsion ThreeSatellite Coulomb Formation in Geostationary Orbit [J]. Aerospace Contrd and Application, 2021, 47(1): 15-21.
[5]	LU Ming, LIANG Zhulin, XU Zhangfan. Dynamic Modeling and Control of Flexible Support Control Moment Gyroscope [J]. Aerospace Contrd and Application, 2021, 47(1): 40-46.
[6]	YAN Han, HE Ying-Zi. DragTracking Guidance for Entry Vehicles with Finite Time [J]. , 2018, 44(1): 38-44.
[7]	XUE Chao, TAN Shu-Ping, LIU He-Long. Librational Controller Design for a Tethered Satellite System during Orbital Maneuvering [J]. , 2017, 43(2): 21-27.
[8]	GENG Jie, 吕Nan , WANG Tao, GONG Jing-Gang. A Novel FiniteTime Sliding Mode Attitude Controller for Spacecraft [J]. , 2016, 42(4): 30-.
[9]	XU Wei, WU Hai-Lei, LU Shan, LIU Fu-Cheng. A High Precision Attitude Tracking Control Method for Highly Eccentric Orbit Spacecraft Rendezvous with a HEO Target [J]. , 2015, 41(2): 6-11.
[10]	WANG Zhi-Gang, YAN Ye-Hui, ZHOU Jia-Xing, DENG Yi-Fan. Hybrid Attitude Control Law for Space Platform [J]. , 2014, 40(1): 9-.
[11]	ZHONG Chen-Xing, GUO Yu, ZHOU Chuan, CHEN Qing-Wei. On Sliding Mode Variable Structure Control and Chattering Reduction for Flexible Spacecraft [J]. , 2013, 39(2): 24-29.
[12]	XING Jian, QI Rui-Yun. Adaptive Sliding-Mode Attitude Control of Spacecraft with Fuel Sloshing [J]. , 2013, 39(2): 42-47.
[13]	HU Min, ZENG Guo-Qiang. FiniteTime Control for Satellite Formation Flight [J]. , 2012, 38(1): 23-28.
[14]	LI Huifeng，SUN Wenchong. Index Approach Law Based Sliding Control for A Hypersonic Vehicle LI Huifeng，SUN Wenchong [J]. , 2009, 35(4): 39-43.
[15]	LIU Zhiyong1,2, HE Yingzi1,2. Integral Sliding Mode Control with Adaptive Parameters for Flying around Slowly Rotating Target [J]. , 2009, 35(4): 22-26.

Sliding Mode Control for Rate Damping of Underactuated Spacecraft

PDF (PC)

Like

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Metrics

Comments

Recommended 0