moreover, the practicability of the normal acceleration feedback is analyzed.
分析了选用法向过载控制回路的合理性。
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。
it can realize the normal acceleration control that the pitch rate feedback is regarded as inner-loop and the normal acceleration feedback is the outer-loop.
以某飞机为研究对象,通过在俯仰角速度控制回路上加上法向过载回路作为外回路,实现飞机纵向控制中的法向过载设计。