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问题。

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This paper deals with the near-minimum-time attitude maneuver control of vertical launching tactical missile, in order to solve fast attitude maneuver of this kind of missile.

针对战术导弹垂直发射姿态调转时的快速性要求，研究了垂直发射快速姿态调转的次最小时间控制问题。

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