文件名称:model
- 所属分类:
- 其他小程序
- 资源属性:
- [Matlab] [源码]
- 上传时间:
- 2017-09-09
- 文件大小:
- 443kb
- 下载次数:
- 0次
- 提 供 者:
- Nicle*****
- 相关连接:
- 无
- 下载说明:
- 别用迅雷下载,失败请重下,重下不扣分!
介绍说明--下载内容均来自于网络,请自行研究使用
本程序可以仿真四旋翼飞行器的飞行,可以设计飞行器控制律,完整的,可以使用,环境是MATLAB(This program can simulate the flight of the four rotor aircraft, you can design aircraft control law, complete, you can use, the environment is MATLAB)
相关搜索: 四旋翼matlab控制
(系统自动生成,下载前可以参看下载内容)
下载文件列表
model\angle_cal.m
model\bianshi.sid
model\convert.m
model\expfuc.asv
model\expfuc.m
model\get_desired_rate.m
model\get_I.m
model\get_I_parameters.m
model\get_output_duty.asv
model\get_output_duty.m
model\get_roll_augumentation.m
model\get_tf.m
model\hs_err_pid6256.log
model\identification_model2.mdl
model\identification_model4.mdl
model\model0.mdl
model\model1.mdl
model\model2.mdl
model\model3.mdl
model\model4.mdl
model\motor.m
model\parameters.asv
model\parameters.m
model\parameters1.m
model\PID_control_attitude_simple1.mdl
model\PID_control_attitude_simple2.mdl
model\PID_control_augmentation.mdl
model\PID_control_debug.mdl
model\PID_control_height.mdl
model\PID_control_PID_augmentation4.mdl
model\PID_control_PID_augmentation5.mdl
model\PID_control_PID_augmentation_function.mdl
model\PID_control_position.mdl
model\PID_control_position2.mdl
model\PID_control_postion_simple.mdl
model\pitch.m
model\pitch_q1.m
model\plotuavtrajectory.m
model\plot_t.m
model\quadrotor_dynamic.asv
model\quadrotor_dynamic.m
model\remote1.m
model\remoteinput.m
model\roll.m
model\roll_p1.m
model\rotor.asv
model\rotor.m
model\rotor1.mdl
model\rotorstate.m
model\runfg.bat
model\state.mdl
model\theta.mdl
model\theta_1.mdl
model\thrust.m
model\thrust1.m
model\thrust_cal.m
model\trim_model.m
model\uper.m
model\visu.mdl
model\yaw.m
model\yawn.txt
model\yaw_r1.m
model
model\bianshi.sid
model\convert.m
model\expfuc.asv
model\expfuc.m
model\get_desired_rate.m
model\get_I.m
model\get_I_parameters.m
model\get_output_duty.asv
model\get_output_duty.m
model\get_roll_augumentation.m
model\get_tf.m
model\hs_err_pid6256.log
model\identification_model2.mdl
model\identification_model4.mdl
model\model0.mdl
model\model1.mdl
model\model2.mdl
model\model3.mdl
model\model4.mdl
model\motor.m
model\parameters.asv
model\parameters.m
model\parameters1.m
model\PID_control_attitude_simple1.mdl
model\PID_control_attitude_simple2.mdl
model\PID_control_augmentation.mdl
model\PID_control_debug.mdl
model\PID_control_height.mdl
model\PID_control_PID_augmentation4.mdl
model\PID_control_PID_augmentation5.mdl
model\PID_control_PID_augmentation_function.mdl
model\PID_control_position.mdl
model\PID_control_position2.mdl
model\PID_control_postion_simple.mdl
model\pitch.m
model\pitch_q1.m
model\plotuavtrajectory.m
model\plot_t.m
model\quadrotor_dynamic.asv
model\quadrotor_dynamic.m
model\remote1.m
model\remoteinput.m
model\roll.m
model\roll_p1.m
model\rotor.asv
model\rotor.m
model\rotor1.mdl
model\rotorstate.m
model\runfg.bat
model\state.mdl
model\theta.mdl
model\theta_1.mdl
model\thrust.m
model\thrust1.m
model\thrust_cal.m
model\trim_model.m
model\uper.m
model\visu.mdl
model\yaw.m
model\yawn.txt
model\yaw_r1.m
model