绳系系统轨道机动过程中的面内摆角抑制

doi:10.3969/j.issn.1674-1579.2017.02.004

Abstract

Abstract: A controller is designed to restrain the inplane libration of a tethered satellite system (TSS). To stabilize the inplane subsystem of TSS, a hierarchical iterative nonlinear sliding mode control is proposed. The stability of the closedloop system is also proved. The validity of the proposed algorithm is demonstrated by numerical simulation results. Moreover, the advantages of the algorithm are presented via comparing with the traditional hierarchical sliding mode control.

Key words: tethered satellite system, sliding mode control, orbital maneuvering

CLC Number:

V448

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.

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URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2017.02.004

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2017/V43/I2/21

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[5]	YAN Han, HE Ying-Zi. DragTracking Guidance for Entry Vehicles with Finite Time [J]. , 2018, 44(1): 38-44.
[6]	GENG Jie, 吕Nan , WANG Tao, GONG Jing-Gang. A Novel FiniteTime Sliding Mode Attitude Controller for Spacecraft [J]. , 2016, 42(4): 30-.
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[8]	GUO Chaoli, ZHANG Duzhou, WANG Shuyi. Sliding Mode Control for Rate Damping of Underactuated Spacecraft [J]. , 2013, 39(4): 12-17.
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[12]	LI Huifeng，SUN Wenchong. Index Approach Law Based Sliding Control for A Hypersonic Vehicle LI Huifeng，SUN Wenchong [J]. , 2009, 35(4): 39-43.
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Librational Controller Design for a Tethered Satellite System during Orbital Maneuvering

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