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Development of Autopilot system of Unmanned Aerial Vehicle for Aerial Mapping Application

机译:航空制图用无人机自动驾驶系统的研制

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The Autopilot of Unmanned Aerial Vehicle (UAV) is a system with the capability of controlling roll, pitch, and yaw of UAV. It also capable to maintain the altitude of UAV automatically. Moreover, it assists UAV travel according to the waypoints and take-off/landing automatically. The features of Autopilot become important to support UAV tasks such as aerial mapping activities, territorial monitoring, and tourism documentation. The paper presents development of GPS-based UAV autopilot system that has several flying modes: (1) stabilize (user manually controls the movement of the aircraft using remote controller, the balance of the aircraft is automatically maintained by the autopilot), (2) automatic (the aircraft automatically flies along the waypoint), (3) take-off/landing (the plane lands and takeoff automatically). The proposed system is developed using Arduino Mega 2560 as the main controller to acquire sensor data, control the roll, pitch, and yaw of the plane, calculate the heading of the plane, and obtain the signal control to the servo motors. The sensors consist of an Inertial Measurement Unit (IMU) of MPU 6050 type, ultrasonic, barometer sensor of BMP 180, magnetometer, and GPS. The system uses Proportional Integral Derivative (PID) controller to maintain the position of the plane (roll, pitch, and yaw) and the altitude. Landing mode uses ultrasonic sensors to measure the altitude of the aircraft when the altitude is less than 3 meters. The proposed system has been successfully implemented and tested. The maximum error during waypoint mode is 50 meters.
机译:无人机自动驾驶仪(UAV)是一种能够控制无人机的侧倾,俯仰和偏航的系统。它还能够自动保持无人机的高度。而且,它可以根据航路点自动协助无人机飞行,并自动起飞/降落。自动驾驶仪的功能对于支持无人机任务(例如空中测绘活动,领土监视和旅游文献)非常重要。本文介绍了基于GPS的无人机自动驾驶系统的开发,该系统具有几种飞行模式:(1)稳定(用户使用遥控器手动控制飞机的运动,自动驾驶仪自动保持飞机的平衡),(2)自动(飞机自动沿着航路点飞行),(3)起飞/降落(飞机自动降落和起飞)。拟议的系统是使用Arduino Mega 2560作为主要控制器开发的,以获取传感器数据,控制飞机的侧倾,俯仰和偏航,计算飞机的航向并获得对伺服电机的信号控制。传感器由MPU 6050型的惯性测量单元(IMU),超声波,BMP 180的气压计传感器,磁力计和GPS组成。该系统使用比例积分微分(PID)控制器来维持飞机的位置(侧倾,俯仰和偏航)和高度。降落模式使用超声波传感器在高度小于3米时测量飞机的高度。所建议的系统已成功实施和测试。航点模式下的最大误差为50米。

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