摘要
航天器交会对接物理仿真是进行交会对接技术地面试验和验证的一种行之有效的方式,本文初步分析了利用微小卫星五自由度仿真平台M icroSim实现交会对接过程中测量方案、制导和控制策略以及GNC软件系统性能等仿真验证的物理仿真系统的可能性,简要介绍了M icroSim仿真平台,提出基于M icroSim仿真平台的航天器交会对接物理仿真系统总体方案。为建立我国的RVD物理仿真系统提供了一条快速低廉的有效途径。
Establishing ground physical simulation system for spacecraft rendezvous and docking is an effective way of studying and validating RVD technologies. This paper elementarily investigates the possibility of using a 5 degree-of-freedom air-bearing testbed, called MicroSim, to validate the monocular vision-based guidance, navigation and control scheme for near-proximity and docking operations. The MicroSim is described, and the scheme of physical simulation system for spacecraft RVD using MicroSim facility is proposed. This paper provides a reference of Chinese spacecraft RVD mission.
出处
《航天控制》
CSCD
北大核心
2006年第2期63-67,96,共6页
Aerospace Control
