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对卫星柔性对接补加一体化机构建模与设计 被引量:4
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作者 黄剑斌 黄龙飞 +4 位作者 韩旭 蒙波 李志 王文龙 李文 《空间控制技术与应用》 CSCD 北大核心 2018年第5期30-37,共8页
阐述了一种弱撞击交会条件的对接补加一体化机构.在机构设计上采用柔性杆实现软连接,刚性周边杆实现纠偏和刚性锁紧,阻尼装置吸收对接碰撞能量,并采用可浮动的气/液耦合和电气接口进一步实现高精度的气/液/电路连接.采用拉格朗日分析力... 阐述了一种弱撞击交会条件的对接补加一体化机构.在机构设计上采用柔性杆实现软连接,刚性周边杆实现纠偏和刚性锁紧,阻尼装置吸收对接碰撞能量,并采用可浮动的气/液耦合和电气接口进一步实现高精度的气/液/电路连接.采用拉格朗日分析力学建立飞行器多体动力学模型,利用模态叠加法对碰撞过程柔性部件的变形进行描述,从而建立飞行器柔性对接动力学模型.多工况动力学仿真试验表面所设计的对接补加一体化机构可在0.25 m/s弱撞击速度范围,20 mm横向对接容差以及±5°角度容差范围内实现可靠对接.对接补加一体化装置完成样机研制,并在直线运动平台上完成对接性能和电路连接的多次试验,在专用补加系统上完成接口密封性和模拟推进剂传输试验. 展开更多
关键词 对接补加 柔性锥杆式机构 柔性动力学建模 弱撞击对接
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Dynamic simulation of a flexible spinning vehicle with the periodic varying thrust 被引量:2
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作者 朱怀亮 余磊 +1 位作者 梁思辉 胡开封 《Journal of Shanghai University(English Edition)》 CAS 2008年第2期115-119,共5页
The dynamic response of a flexible spinning vehicle with the varying thrust was investigated. The varying thrust was modeled as a series of simple harmonic components superimposed on a constant thrust. The analytical ... The dynamic response of a flexible spinning vehicle with the varying thrust was investigated. The varying thrust was modeled as a series of simple harmonic components superimposed on a constant thrust. The analytical solutions for longitudinal motion were obtained by combining the motion equations and boundary conditions, and then, the transverse bending of rocket was examined solved by considering a coupled forcing vibration with varying parameters. Numerical solutions for a rocket with end-varying thrust were studied. It is shown that the lateral vibrations and motion attitudes of rocket depend on the frequencies of varying thrust to great extent, and an important phenomenon, beating, maybe take place. The proposed approach is more accurate and efficient in comparison to those standard numerical techniques. 展开更多
关键词 dynamics flexible vehicle varying thrust semi-analytical method.
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