摘要
研究了航天器与空间站对接过程的建模与控制问题。建立包括质心运动、刚体姿态运动和挠性结构弹性振动的对接系统的全面运动数学模型，分析了对接控制中需要注意的几个问题和具体的控制方案，最后通过计算机仿真说明了该控制方案的有效性。
The paper mainly studies the modeling and control problem of spacecrafts' docking process. The complete mathematical model of docking system is established, which includes centroid movement of spacecraft, attitude movement of rigid body and elastic vibration of flexible structure. Then the concrete control scheme is formulated, and computer simulation of the whole process is made to show the effectiveness of the given method.
出处
《系统仿真学报》
EI
CAS
CSCD
2001年第3期280-283,共4页
Journal of System Simulation
