Optimal control of tactical maneuver for a high-performance aircraft is investigated in flight trajectory.
应用轨迹优化方法研究了高性能战斗机机动动作的最优控制问题。
The time-optimal control law for motor torques of reaction wheels is designed, and, the calculated formulations of maneuver time and system state are given.
进一步的设计了反作用飞轮电机力矩的快速控制规律。给出了机动时间和系统状态的简单计算公式。
An optimal orbit maneuver method based on continuous low thrust was presented to solve relative motion control.
针对近距离相对运动的轨道控制问题，提出用常值小推力完成最优转移的方法。
An optimal orbit maneuver method based on continuous low thrust was presented to solve relative motion control.
针对近距离相对运动的轨道控制问题，提出用常值小推力完成最优转移的方法。
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