This paper studies the attitude large Angle slew problem that rate and control moment of the lunar probe are limited.
研究了月球探测器转速与控制力矩受限的姿态大角度机动问题。
Based on idea of time scale, an attitude large Angle slew control method is presented.
根据时间变尺度思想，提出了双回路反馈的姿态大角度机动控制方法。
This paper is concerned with the dynamics and control for planar, large Angle rapid slew maneuvering of a flexible multi body spacecraft, consisting of a rigid central body and a flexible beam.
研究一类构形为中心刚性带挠性梁的航天器平面快速大角度机动的动力学与控制问题。
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