Publisher
Springer Science and Business Media LLC
Reference22 articles.
1. KUANG J L, MEEHAN P A, LEUNG A Y T, et al. Nonlinear dynamics of a satellite with deployable solar panel array [J]. International Journal of Non-Linear Mechanics, 2004, 39: 1161–1179.
2. KOTE A, BALAJI K, NATARAJU B S, et al. Effect of solar array deployment on spacecraft attitude [J]. Journal of Spacecraft Technology, 2007, 17(2): 1–8.
3. BAI Z F, ZHAO Y. Attitude motion of spacecraft during oblique solar panel deployment [J]. Aircraft Engineering and Aerospace Technology, 2012, 84(2): 109–114.
4. KOJIMA Y, TANIWAKI S, OKAMI Y. Dynamic simulation of stick-slip motion of a flexible solar array [J]. Control Engineering Practice, 2008, 16(6): 724–735.
5. DING X L, LI X, XU K, et al. Study on the behavior of solar array deployment with root hinge drive assembly [J]. Chinese Journal of Aeronautics, 2012, 25(2): 276–284.
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