1) attitude adjuster
姿态调节器
1.
Considering the character of missile attitude control system, a design method and a control algorithm of missile attitude adjuster are proposed,and theoretical basis for actual application is provided.
将工程中常用的"分段定常"方法与全程滑态变结构控制理论相结合,提出了独特的时变全程滑态变结姆控制方法,并结合导弹姿态控制系统特点,提出了导弹姿态调节器设计方法和导弹姿态调节器控制算法,为实际应用提供了一定的理论基础与依据。
2) attitude regulation
姿态调节
1.
Satellite attitude regulation control subject to control Input saturation;
考虑控制输入饱和的卫星姿态调节控制
2.
Adaptive sliding mode controller design for satellite attitude regulation;
卫星姿态调节的自适应滑模控制器设计
3.
A sliding mode PID controller design for satellite attitude regulation;
卫星姿态调节的滑模PID控制器设计
3) attitude regulation of a rigid body
刚体姿态调节
1.
Two control laws are presented for attitude regulation of a rigid body expressed by unit quaternion.
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 。
5) fine adjustment of attitude
姿态微调
6) attitude adjustment
姿态调整
1.
This paper is based on the necessary condition and sufficient condition for the balance of any space force system in static mechanics,in combination with the structural properties of the actual target attitude suspending control system,the mathematical model for attitude adjust