摘要
论述了一种用于火箭推力矢量控制系统中的三余度伺服机构 ,介绍了其工作原理 ,并对其进行了数学仿真分析及试验验证。
A kind of triplex redundant servomechanism for rocket thrust vector control is described. The operating principle of the servomechanisim is introduced,and the result of performance simulation and experiment is presented.
出处
《导弹与航天运载技术》
2000年第2期14-16,共3页
Missiles and Space Vehicles
