PID control algorithm for three attitude angles of helicopter
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文件大小： 36KB
中文说明：
直升机的三个姿态角的pid控制算法，matlab中的simulink仿真程序，配合最优pid设计算法，得到很好的控制效果。
English Description：
The PID control algorithm of helicopter's three attitude angles, the Simulink simulation program in MATLAB, with the optimal PID design algorithm, get good control effect.
姿态角控制-PID
..............\Attitude_angle_controller
..............\.........................\gen.m
..............\.........................\phi_control.mdl
..............\.........................\phi_control_pd.mdl
..............\.........................\theata_control.mdl
..............\height_control
..............\..............\height_control.mdl
..............\leading_control
..............\...............\leading_control.mdl