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|Title:||Decentralized sliding-mode control for attitude synchronization in spacecraft formation||Authors:||Wu, Baolin
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
|ISSN:||1049-8923||DOI:||http://dx.doi.org/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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