文件名称:pingying_v57
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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,这个有中文注释,看得明白,IMC-PID是利用内模控制原理来对PID参数进行计算。- It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle, The Chinese have a comment, understand it, The IMC- PID is using the internal model control principle for PID parameters is calculated.
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pingying_v57.m