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Description: UAV 自动驾驶的，无人飞行机器人控制源码。-UAV autopilot, flying unmanned robot control source.
Platform: |
Size: 759215 |
Author: 王虎林 |
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Description: UAV 自动驾驶的，无人飞行机器人控制源码。-UAV autopilot, flying unmanned robot control source.
Platform: |
Size: 758784 |
Author: 王虎林 |
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Description: 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
Platform: |
Size: 2048 |
Author: liying |
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Description: 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.
Platform: |
Size: 14336 |
Author: gaojubin |
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Description: 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.
Platform: |
Size: 57344 |
Author: yuanfang |
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