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本文全面推导了飞机对连续大气紊流的加速度(包括三个线加速度和三个角加速度)响应的传递函数和功率谱,为正确计算各加速度的均方根提供了数学依据,为进一步分析计算突风减缓控制系统打下必要的基础。
This paper comprehensively deduces the transfer function and power spectrum of the aircraft response to the continuous atmospheric turbulence acceleration (including the three linear accelerations and the three angular accelerations), and provides a mathematical basis for correctly calculating the root mean square of each acceleration. For further analysis and calculation Gust mitigation control system to lay the necessary foundation.