The optimization requires the minimization of the normal acceleration overload at the position of pilot, the attitude variation and the control energy consumption under gust disturbance.
优化性能指标要求在阵风扰动下驾驶员处法向过载、飞机姿态变化、以及控制信号能量损耗最小。
The LQ is adapted to the flight control law design such as the Normal Acceleration control system.
并以法向过载控制模态为例，将线性二次型运用到飞行控制系统的控制律设计中。
The LQ is adapted to the flight control law design such as the Normal Acceleration control system.
并以法向过载控制模态为例，将线性二次型运用到飞行控制系统的控制律设计中。
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