摘要
遥操作交会对接是指操作人员在远端通过遥操作方式控制追踪航天器进行交会对接,主要用于无人航天器自动交会对接系统故障条件下平移靠拢段的交会对接控制。简要介绍了遥操作交会对接的基本概念及其国内外研究现状;结合我国载人航天工程的基本特点,设计了适用于我国未来空间站任务的遥操作交会对接系统;根据设计的系统方案,设计和开发了相应的遥操作交会对接仿真系统,并进行了部分仿真分析和遥操作交会对接试验,初步验证了设计方案的可行性。
Teleoperation rendezvous and docking is referred to as the concept that the chase spacecraft is flown distantly through teleoperation approach. It can be used as a backup for autonomous rendezvous and docking for the unmanned chases during the finally approach stage. The concept of teleoperation rendezvous and docking （RVD） and the previous studies in this field were introduced firstly. Then, a design of the teleoperation RVD system was addressed, which is based on the primary assumed conditions of our future space station project. Finally, a simulation system was developed and corresponding experiments were carried out for verifying the design, especially the design with teleoperation time delay. The results show that the design is feasible, even though there are jobs to be done in the future.
出处
《国防科技大学学报》
EI
CAS
CSCD
北大核心
2012年第3期24-28,共5页
Journal of National University of Defense Technology
基金
国家部委资助项目
关键词
遥操作交会对接
系统设计
仿真分析
时延
teleoperation rendezvous and docking
system design
simulation analysis
time delay
