1) orbit and attitude control section body for missile
导弹轨姿控舱体
1.
Analysis on strength of the orbit and attitude control section body for missile;
导弹轨姿控舱体的强度分析
2) missile attitude control
导弹姿态控制
1.
A design method of discrete variable structure control with fast output sampling(FOS) feedback technique and a new control law was proposed to solve the control of missile attitude control system in this paper.
针对导弹姿态控制系统这一多输入多输出、具有参数时变和不确定干扰的离散时间线性系统,采用快速输出采样技术,设计了一种离散变结构控制器,给出了改进的自适应离散趋近律,要求未知扰动有界,但不要求满足匹配条件。
2.
The result showed that the controller had satisfactory effect when using in simulation of digital missile attitude control system.
针对数字式导弹姿态控制系统的参数具有时变性和不确定性的特点,设计了一种离散变结构控制器。
3) missile GCU
导弹制导控制舱
4) Attitude and Orbit Control
姿轨控
1.
Attitude and Orbit Control subsystem which is an important part of a satellite attitude control system is the core components to achieve high-performance attitude and orbit measurement and control.
姿轨控下位机作为卫星姿轨控分系统的重要组成部分,是卫星实现高性能姿轨测量和控制的核心部件。
5) Missile Attitude
导弹姿态
1.
Three-axes Missile Attitude Based on Star Sensor;
星敏感器测量导弹姿态的方法研究
6) missile attitude control system
导弹姿态控制系统
1.
In the research of fault detection and diagnosis for the missile attitude control system,the BP neural network has the disadvantages such as slow convergence.
在导弹姿态控制系统的故障检测和诊断中,针对BP神经网络自身存在的收敛速度慢等缺点,介绍了一种新型神经网络——带偏差单元的递归神经网络的结构及算法。
补充资料：姿体
1.相貌，身材。
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