Author:
Li Hai-Quan,Duan Liu-Cheng,Liu Xiao-Feng,Cai Guo-Ping
Funder
National Natural Science Foundation of China (CN)
Shanghai Municipal Education Commission (CN)
Natural Science Foundation of Shanghai (CN)
Special Fund for Talent Development of Minhang District of Shanghai
Publisher
Springer Science and Business Media LLC
Subject
Control and Optimization,Computer Science Applications,Mechanical Engineering,Aerospace Engineering,Modelling and Simulation
Reference16 articles.
1. Wie, B., Furumoto, N., Banerjee, A.K., Barba, P.M.: Modeling and simulation of spacecraft solar array deployment. J. Guid. Control Dyn. 9(5), 593–598 (1986)
2. Wallrapp, O., Wiedemann, S.: Simulation of deployment of a flexible solar array. Multibody Syst. Dyn. 7(1), 101–125 (2002)
3. Kojima, Y.: Attitude vibration caused by a stick-slip motion for flexible solar array of advanced Earth observation satellite. J. Vib. Control 10(10), 1459–1472 (2004)
4. Kote, A., Balaji, K., Nataraju, B.S.: Aralimatti VC. Effect of solar array deployment on spacecraft attitude. J. Spacecr. Technol. 17(2), 1–8 (2007)
5. Kwak, M.K., Heo, S., Kim, H.B.: Dynamics of satellite with deployable rigid solar arrays. Multibody Syst. Dyn. 20(3), 271–286 (2008)
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