介绍了变体飞行器控制系统和涉及的控制理论问题。
The control system and related control theory of morphing aircraft are introduced.
姿态控制推力器(act)是飞行器控制系统的执行部件。
The attitude control thruster (ACT) is the control component of the flight vehicle.
文中给出了一个弹性飞行器的姿态控制系统作为设计举例。
An example of an attitude control system of a bending vehicle is given.
文中给出了一个弹性飞行器的姿态控制系统作为设计举例。
An example of an attitude control system of a bending vehicle is given.
应用推荐