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《Missiles and Space Vehicles》 2002-06
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Effects of Clearances on Dynamic Performances of Deployable Structures for Spacecraft

Yan Shaoze Ye Qing Shen Yongsheng Chen Hongbin(Department of Precision Instruments and Mechanology,Tsinghua University, Beijing, 100084)$$$$  
Based on contact deformation mode of clearance′s joints, dynamic equations of the deployable structures with clearances is developed to find out the influences on dynamic performances of the structure for spacecraft. Dynamics of a typical deployable structure with a clearance is simulated, and the simulation results show that dynamic performances of the structure are greatly influenced by the clearance during deploying. At beginning, there are bigger contact forces, and then come into being impulse impact forces continuously. As dimensions of the clearance increase, amplitudes of impact forces are trend to increase and times of impacts decrease. Frictions could result in non linear dynamic response, but at the same time, they could have effects on suppressing dynamic disturbances for the deployable structure.
【Fund】: 国家航天 86 3高技术项目 ( 86 3-2 -2 -4 -2 );; 国家自然科学基金 ( 5 990 5 0 1 6 )资助
【CateGory Index】: V414
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