空间交会对接的仿真技术  

SIMULATION TECHNOLOGY FOR RENDEZVOUS AND DOCKING IN SPACE

作　　者：林来兴[1] 

机构地区：[1]北京控制工程研究所

出　　处：《航天控制》1990年第4期66-71,21,共7页Aerospace Control

摘　　要：空间交会对接涉及到两个航天器同时要进行多达12个自由度的轨道和姿态控制问题。这不仅在理论上,而且在技术实现上都是相当复杂的。为了确保交会对接的成功并尽量缩短交会对接的时间,必须用实际硬件和星上软件进行整个RVD控制系统的仿真试验。本文主要论述对交会对接仿真技术的要求,仿真方法和关键仿真设备。The rendezvous and docking (RVD) between two spacecrafts in space in-volves both orbit control and attitude control with up to 12 degrees of freedom. It is very com-plex not only in theory but also inimplementation. In order to ensure the success for RVD and minimize the time for RVD, it is necessary f or simulation testing of complete RVD controlsystem with real hardware and onboard software in the loop. This paper primarily discusses the specification of RVD simulation, simulation methodsand critical simulation equipments.

关 键 词：交会 对接 仿真技术 空间 

分 类 号：V526[航空宇航科学与技术—人机与环境工程]