刚体的姿态可以用不同的参数来描述，由此可以产生不同的控制方法。
The attitude of a rigid body can be described by different parameters , hence it yields different control methods.
给出了用四元数表示的刚体姿态调节问题的两种控制规律。
Two control laws are presented for attitude regulation of a rigid body expressed by unit quaternion.
研究了刚体飞行器大角度机动的姿态控制问题。
In this paper, attitude control problem of a rigid spacecraft with large Angle maneuvers is investigated.
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