2) launch vehicle attitude control system
火箭姿态控制
1.
This paper introduces the working principle of servomechanism in the launch vehicle attitude control system and puts forward the possibility that hydraulic accumulator is directly used as the driver of the launch vehicle attitude servo control system, based on the working characteristics of servomechanism, and the problems to solve.
本文介绍了火箭姿态控制伺服机构的工作原理,并根据伺服机构在火箭姿态控制系统中的工作特点,提出了用液压蓄能器直接作为火箭姿态控制系统伺服机构动力源的可能性以及需要解决的问题。
3) flexible satellite attitude control
柔性卫星姿态控制
5) flexible rocket
柔性火箭
6) Launch vehicle
运载火箭
1.
Fault diagnosis technology of launch vehicle based on distributed expert system;
基于分布式专家系统的运载火箭故障诊断技术
2.
Modeling and Simulation of Navigation Calculating Subsystem of Launch Vehicle;
运载火箭导航计算子系统建模与仿真
3.
Onboard real-time compression of launch vehicle telemetry images;
运载火箭飞行状态图像箭上实时压缩技术研究
补充资料：柔性
1.柔顺之性。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条