attitude maneuver

基本解释

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。
Based on near-eigenaxis decomposition theorem of the relative attitude, the control law of relative attitude maneuver based on quaternion is designed and simulated.
根据相对姿态的欧拉轴分解定理，设计了基于四元数反馈的相对姿态机动控制律，并对相对姿态控制律进行了仿真分析。
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。