A modified sliding mode fault tolerant controller is developed for flexible spacecraft attitude stabilization control in the presence of loss of actuator effectiveness fault and actuator stuck fault.
针对挠性航天器执行器卡死与失效故障的姿态稳定控制问题，提出了一种结构简单、计算量小的改进型滑模容错控制策略。
The core of stabilization platform is the attitude measurement and control of the carrier.
稳定平台的核心问题是载体姿态测量和控制技术。
The stratospheric nacelle attitude control system is the key technology in keeping position stabilization and posture adjustment.
气球吊篮姿态控制系统是吊篮在空中保持姿态稳定、进行姿态调整的关键部件。
The self-learning fuzzy control based on sliding mode control is applied to the attitude stabilization of flexible satellites.
将基于滑模控制的自学习模糊控制应用于挠性卫星的姿态稳定控制中。
The control algorithm of attitude follow-up stabilization and tracking antenna platform adopts position feed-forward control, speed control and position feedback control.
姿态随动稳定跟踪天线平台的控制算法，采用位置前馈、速度和位置反馈控制。
The attitude control of 3-axis stabilization satellite was studied under the disturbance due to the movement of payload in this paper.
研究了考虑有效载荷运动部件干扰时三轴稳定卫星的姿态控制。
The attitude control of 3-axis stabilization satellite was studied under the disturbance due to the movement of payload in this paper.
研究了考虑有效载荷运动部件干扰时三轴稳定卫星的姿态控制。
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