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本文研究航天器运动控制的姿态定向模式与轨道校正模式的优化协调问题。既研究了解决该问题的一般方法,又具体提出了航天器的旋转及轨道运动的协调控制问题。文中给出了空间站适用的与轨道校正相协调进行的航天器姿态重新定向控制的具体算法。表明了航天器姿态定向与轨道高度保持协调控制有高效率。列举了两种发动机安装模式的数学仿真实例,给出了效率指数的评估值以及旋转次数确定时算出的校正速度值。
This paper studies the optimization and coordination of attitude-oriented mode and orbital correction mode of spacecraft motion control. Both the general method of solving this problem is studied, and the coordinated control of the rotation and orbital motion of the spacecraft is also specifically proposed. In this paper, the specific algorithm of spacecraft attitude reorientation control which is suitable for orbital correction is given. It shows that there is high efficiency in coordination control of spacecraft attitude and orbit height. The examples of mathematical simulation of two engine mounting modes are given. The evaluation values of the efficiency index and the correction speed values obtained when the rotation times are determined are given.