摘要
针对载人航天器"人在回路"的特点,在评价现有人控交会对接试验系统特点的基础上对地面验证系统设计原则进行归纳,提出一种载人航天器人工控制系统地面验证平台设计方案.该方案在继承以往航天器自动控制系统地面测试系统设计要点的基础上将"人"纳入控制闭环中,确保了载人航天器人工控制系统地面验证真实性.最后对平台的信息流回路、光学变换器等关键技术进行了阐述.
The existing test systems for manual-control rendezvous and docking technique are reviewed. Based on the characteristics of man-in-the-loop for a manned spacecraft, the design principle of ground verification system is thoroughly studied. As a result, a general design scheme is established. In this design, the essential elements of the conventional ground verification system for spacecraft autocontrol systems are kept, and man is included in the control loop as well. Finally key techniques such as man-based data link, optical converter and so on are described.
出处
《空间控制技术与应用》
2010年第4期50-53,共4页
Aerospace Control and Application
关键词
人工控制
交会对接
模拟座舱
视景
光学变换器
manual-control
rendezvous and docking
simulation cabin
virtual vision
optical converter