本文导出了基于对象CARMA模型的多变量广义预测自适应控制器，并将这种新的控制方法应用于航天器轨道控制中。
It is presented in this paper a multivariable generalized predictive adaptive controller based on CARMA model and its application in the orbit control of spacecraft.
空间交会对接涉及到两个航天器同时要进行多达12个自由度的轨道和姿态控制问题。
The rendezvous and docking (RVD) between two spacecrafts in space involves both orbit control and attitude control with up to 12 degrees of freedom.
最后，采用轨道根数作为状态变量，以航天器发动机产生的推力加速度作为控制变量建立空间拦截模型。
Finally, the orbital elements are introduced as state variables and the accelerations are produced by equation as control variables, the space interception model is established.
研究小偏心参考轨道航天器编队飞行构形保持与重构控制的工程实现技术。
In this paper, the enabling technique of maintenance and reconfiguration control of spacecraft formation flying is studied.
研究搭载在空间站或其他近地轨道航天器上的空间模块化机械手系统的容错控制系统。
This paper studies a fault-tolerant control system for a space modular manipulator system mounted on space station or other spacecrafts such as satellites, located in low earth orbit.
本文介绍了将智能控制方法用于航天器交会对接段的轨道控制。
The method of intelligent control applied to the orbital control of rendezvous and docking phase of spacecraft is presented in this paper.
本文介绍了将智能控制方法用于航天器交会对接段的轨道控制。
The method of intelligent control applied to the orbital control of rendezvous and docking phase of spacecraft is presented in this paper.
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