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.
从时域内对存在模型误差的弹性飞行器控制系统进行了稳定鲁棒性研究。
The stability robustness for uncertain system models of elastic vehicles is studied in time-domain.
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