摘要
本文介绍了大型捆绑运载火箭姿态控制系统方案、工作原理和首发飞行试验结果,并将部分参数同美国航天飞机进行比较。
This paper introduces in detail the scheme and principle of the attitude control system of a large-scale launch vehicle in which four boosters are strapped-on and flight test results. A part of parameters of system are compared with that of the Americal Space Shuttle.
出处
《航天控制》
CSCD
北大核心
1991年第1期1-6,共6页
Aerospace Control
关键词
姿态控制系统
运载火箭
捆绑火箭
Attitude control system
^+Attitude angle rate control loop
^+Mass center
Artificial intelligence
Space shuttle
