This article investigates the spacecraft autonomous attitude maneuver control in the presence of forbidden attitude. 主要研究存在禁止姿态的航天器自主姿态机动控制(MC)问题。
In this paper, the issue on fast attitude maneuver control of a spacecraft with flexible appendix is studied. 研究带柔性附件航天器的姿态快速机动控制(MC)问题。
The multi-target rapid maneuver control problem is studied for agile satellites with Variable Speed Control Moment Gyro ( VSCMG ) as actuator. 研究了以变速控制力矩陀螺(VSCMG)作为执行机构的卫星多目标快速机动的控制问题。
Spacecraft Large Angle Maneuver Control(MC) Based on Inverse Dynamic 基于逆动态理论的空间飞行器大角度机动控制(MC)
Several kinds of terminal tridimensional maneuver control methods were compared in this article, and followed with the analysis of their application situation. 比较了几种末端机动控制(MC)方式的不同,分析了它们的应用场合。