文件名称:hingpan
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IMC-PID是利用内模控制原理来对PID参数进行计算,ML法能够很好的估计信号的信噪比,包含飞行器飞行中的姿态控制,如侧滑角,倾斜角,滚转角,俯仰角。- The IMC- PID is using the internal model control principle for PID parameters is calculated, ML estimation method can be a good signal to noise ratio, It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle
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hingpan.m