Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/102473
Title: Decentralized sliding-mode control for attitude synchronization in spacecraft formation
Authors: Wu, Baolin
Wang, Danwei
Poh, Eng Kee
Keywords: DRNTU::Engineering::Electrical and electronic engineering
Issue Date: 2012
Source: Wu, B., Wang, D., & Poh, E. K. (2012). Decentralized sliding-mode control for attitude synchronization in spacecraft formation. International journal of robust and nonlinear control, 23(11), 1183-1197.
Series/Report no.: International journal of robust and nonlinear control
Abstract: This paper addresses attitude synchronization and tracking problems in spacecraft formation in the presence of model uncertainties and external disturbances. A decentralized adaptive sliding mode control law is proposed using undirected interspacecraft communication topology and analyzed based on algebraic graph theory. A multispacecraft sliding manifold is derived, on which each spacecraft approaches desired time-varying attitude and angular velocity while maintaining attitude synchronization with the other spacecraft in the formation. A control law is then developed to ensure convergence to the sliding manifold. The stability of the resulting closed-loop system is proved by application of Barbalat's Lemma. Simulation results demonstrate the effectiveness of the proposed attitude synchronization and tracking methodology.
URI: https://hdl.handle.net/10356/102473
http://hdl.handle.net/10220/16869
ISSN: 1049-8923
DOI: 10.1002/rnc.2812
Rights: © 2012 John Wiley & Sons, Ltd.
Fulltext Permission: none
Fulltext Availability: No Fulltext
Appears in Collections:EEE Journal Articles

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