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[Other resource] autopilot-2.5.tar DL : 0: UAV 自动驾驶的，无人飞行机器人控制源码。-UAV autopilot, flying unmanned robot control source.
Update : 2008-10-13 Size : 741.42kb Publisher : 王虎林
[Other Embeded program] autopilot-2.5.tar DL : 1: UAV 自动驾驶的，无人飞行机器人控制源码。-UAV autopilot, flying unmanned robot control source.
Update : 2025-02-19 Size : 741kb Publisher : 王虎林
[assembly language] remotreceive DL : 0: 遥控接收解码采用AT89C2051 P1.0-P1.1为电机前后驱动，P1.2-P1.3为左右转弯驱动，P1.4为自动驾驶指示，编码输入从P3.1和p3.2（int0）口，P3.0和P3.5分别为前后红外线探头，在自动驾驶时以控制小汔车前进倒退 -Remote Control Receiver Decoder using AT89C2051 P1.0-P1.1 for before and after the drive motor, P1.2-P1.3 for the driver to turn left or right, P1.4 autopilot instructions for encoding input from P3.1 and p3.2 (int0) I, P3.0 and P3.5, respectively before and after the infra-red probe, while driving in automatic control of small cars, forward regression
Update : 2025-02-19 Size : 2kb Publisher : liying
[assembly language] 2 DL : 0: 遥控接收解码 P1.0-P1.1为电机前后驱动，P1.2-P1.3为左右转弯驱动，P1.4为自动驾驶指示，编码输入从P3.1和p3.2（int0）口，P3.0和P3.5分别为前后红外线探头，在自动驾驶时以控制小汔车前进倒退。-Remote Control Receiver Decoders P1.0-P1.1 for before and after the drive motor, P1.2-P1.3 for the driver to turn left or right, P1.4 for autopilot instructions encoding input from P3.1 and p3.2 (int0) I, P3.0 and P3.5, respectively before and after the infra-red probe, automatic to control when driving smaller cars, move back.
Update : 2025-02-19 Size : 14kb Publisher : gaojubin
[matlab] Simulations-of-Boeing-747 DL : 1: 以波音747为背景，建立了飞机运动的空间六自由度仿真模型。其中包含以下部分： 1. 飞机运动的空间六自由度仿真模型 2. 自动驾驶仪仿真模型； 3.执行器仿真模型； 4.大气重力环境模型； 5.气动数据模型； 6.发动机推力模型；另外，仿真过程中： 1.考虑了风场的影响 2.考虑了传感器的随机噪声； 3.考虑了执行器时间延迟； 4.采用变增益控制器；状态方程选取：速度、攻角、侧滑角、机体系三轴角速度、欧拉角、地面坐标系坐标作为状态量；输出方程有：12个状态量；12个状态微分值；以及机体系速度、加速度、过载等。 -Boeing 747 as the background, the establishment of aircraft motion space six degrees of freedom simulation model. It contains the following sections: 1. Aircraft motion space six degrees of freedom simulation model 2 autopilot simulation model 3. Actuator simulation model 4. Atmospheric gravity environment model 5. Aerodynamic data model 6 engine thrust model Also, the simulation process: 1. considering the impact of the wind farm 2. Consider the sensor random noise 3. considered actuator time delay 4. using variable gain controller equation of state selection: speed, angle of attack , sideslip angle, angular velocity axis machine system, Euler angles, ground coordinates coordinates as state variables output equation are: 12 state variables 12 states differential value and machine system speed, acceleration and overload.
Update : 2025-02-19 Size : 56kb Publisher : yuanfang