Tandem dual-rotor aircraft and flight control method thereof
Tandem dual-rotor aircraft and flight control method thereof
- Neue Suche nach: LIU XINGCHAO
- Neue Suche nach: YANG DAWEI
- Neue Suche nach: LI DONGDONG
- Neue Suche nach: XIE ZHENG
- Neue Suche nach: LIU XINGCHAO
- Neue Suche nach: YANG DAWEI
- Neue Suche nach: LI DONGDONG
- Neue Suche nach: XIE ZHENG
The invention relates to the technical field of unmanned aerial vehicles, in particular to a tandem dual-rotor aircraft and a flight control method thereof, and the method comprises the steps of initializing a flight controller and a sensor, obtaining current attitude information (pitching, rolling and yaw angles), determining expected actions and instructions (pitching, rolling, yawing, ascending and descending) according to input or tasks, and controlling the flight control of the tandem dual-rotor aircraft. The rotating speed difference of the propellers is adjusted to reach the expected angle and height, and the rotating speed is gradually reduced to achieve slow landing. According to the flight control method of the tandem dual-rotor aircraft, propeller rotating speed control and attitude sensor information are combined, and various actions and instructions can be executed.
本发明涉及无人机技术领域，具体是涉及一种纵列双旋翼飞行器及其飞行控制方法，该方法包括初始化飞行控制器和传感器，获取当前姿态信息(俯仰、滚转、偏航角)，根据输入或任务确定期望动作和指令(俯仰、滚转、偏航、上升、下降)，调整螺旋桨转速差异以达到期望角度和高度，逐渐减小转速实现缓慢降落。这种纵列双旋翼飞行器的飞行控制方法结合了螺旋桨转速控制和姿态传感器信息，可执行各种动作和指令。
Dokumentinformationen
Tandem dual-rotor aircraft and flight control method thereof
一种纵列双旋翼飞行器及其飞行控制方法
2023-11-17
Patent
Elektronische Ressource
Chinesisch
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