Control strategy of optimal deployment for spacecraft solar array system with initial state uncertainty
Author:
Publisher
Springer Science and Business Media LLC
Subject
Applied Mathematics,Mechanical Engineering,Mechanics of Materials
Link
http://link.springer.com/article/10.1007/s10483-018-2378-8/fulltext.html
Reference35 articles.
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3. KWAK, M. K., HEO, S., and KIM, H. B. Dynamics of satellite with deployable rigid solar arrays. Multibody System Dynamics, 20(3), 271–286 (2008)
4. ZHANG, D. G. and ZHOU, S. F. Dynamic analysis of flexible-link flexible-joint robots. Applied Mathematics and Mechanics (English Edition), 27(5), 695–704 (2006) https://doi.org/10.1007/s10483-006-0516-1
5. ZHANG, D. G. Recursive Lagrangian dynamic modeling and simulation of mult-link spatial flexi-ble manipulator arms. Applied Mathematics and Mechanics (English Edition), 30(10), 1283–1294 (2009) https://doi.org/10.1007/s10483-009-1008-2
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