摘要
本文提出实现空间飞行器软对接的一种可控的六杆对接装置方案。文中建立了该系统的数学模型,给出了对接口的位置和姿态与控制杆轴向位移的关系,文本还给出一个算例,论证这种软对接方案的可行性。
In this paper, a controllable six-rod docking mechamism concept to implement the soft-docking between two spacecrafts is presented, and the mathematical model of the system is established, which gives the relation of position and attitude of docking port to axial displacements of controlled rods. Finally, a calculated example is given to demonstrate feasibility of the soft-docking concept.
出处
《航天控制》
CSCD
北大核心
1990年第2期44-52,共9页
Aerospace Control
关键词
航天器
对接
动力学
控制
Spacecraft Rendezvous Docking Dynamics Dynamic control ^+Soft docking
