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Alternative TitleDesign of Physical Simulation System for Satellite Flexible Rotating Panels Based on Flotation
尹猛; 徐志刚; 白鑫林; 刘哲
Source Publication空间科学学报
Indexed ByCSCD
Contribution Rank1
Keyword卫星旋转帆板 主轴惯量 挠性频率 动力学等效 振动特性
Other AbstractThe elastic vibration is the main reason that affects the pointing accuracy and control performance of the space vehicle. It is of great interest to verify the ability of the control system to suppress vibration. Because the natural vibration frequency of solar panel is very low and its scale is large, the difficulty and cost to construct a spatial microgravity environment in ground are great. A flexible simulator based on equivalent principal axis inertia and flexible frequency is presented. Based on flotation technique, the physical simulation system of low friction and micro gravity environment is designed, and the dynamic model of the simulator is established, which realizes the effective and high economic test of the control algorithm. The results verify that the vibration characteristics of the simulator is consistent with those of the real solar panel, and its performance meets the test requirements. The simulator can change the parameters smoothly through a simple operation to simulate various flexible satellite rotating panel with different parameter and structure.
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Cited Times:1[CSCD]   [CSCD Record]
Document Type期刊论文
Corresponding Author尹猛
Recommended Citation
GB/T 7714
尹猛,徐志刚,白鑫林,等. 基于气浮的卫星挠性旋转帆板物理仿真系统设计[J]. 空间科学学报,2017,37(3):338-343.
APA 尹猛,徐志刚,白鑫林,&刘哲.(2017).基于气浮的卫星挠性旋转帆板物理仿真系统设计.空间科学学报,37(3),338-343.
MLA 尹猛,et al."基于气浮的卫星挠性旋转帆板物理仿真系统设计".空间科学学报 37.3(2017):338-343.
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