This paper deals with the large Angle attitude maneuver control of spacecrafts.
本文研究空间飞行器大角度姿态机动的控制问题。
This paper investigates the large Angle attitude post stall maneuver control for the agile turn phase of an air-to-air missile that has high off-boresight capability and head reverse maneuverability.
为研究具有大离轴角及越肩发射能力的先进空空导弹初始段敏捷转弯方法，研究了装有反作用喷气控制系统的空空导弹的大角度姿态过失速机动控制律。
The large angle maneuver is one of the key technologies for spacecraft attitude control, which has been the focus of attention.
大角度机动作为现代航天器姿态控制关键技术之一，一直为航天控制领域关注。
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