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REMOTE SENSING TECHNOLOGY USING AN UNMANNED HELICOPTER WITH A CONTROL PAN-HEAD

机译:使用带有控制泛头的无人直升机的遥感技术

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It is difficult that an operator controls an unmanned helicopter to destination (Masanao K., 2003); especially it is far between an operator and helicopter. Because an unmanned helicopter is maneuvered by a radio control system on the ground. The objective of this study is to improve efficiency and accuracy based in pan-head control of remote sensing using an unmanned helicopter. For the unmanned helicopter used in this research, an RTK-GPS was adopted as a positioning sensor, and an inertial sensor that provides posture (roll and pitch angles) was installed in the helicopter. Moreover, a geomagnetic direction sensor (GDS) that outputs and absolute direction is also equipped with the helicopter And the helicopter was installed the pan-head to mount an imaging sensor under the fuselage. That pan-head can rotate two directions (pan and tilt) and equipped rotary encoders to measure the angles. The method for improving remote sensing efficiently is to calculate pan and tilt angles from helicopter position, posture, and target position and to control the pan-head Accuracy of the system was confirmed by a computer simulation. The software also has been developed to support operators and displays helicopter position and posture by 3D graphics. In order to develop the system, we analyzed the pan-head transient and steady-state response and built a dynamic model of the pan-head and get a real helicopter flight data. As the result, RMS error is 27.8cm and maximum error is 2.69m. This accuracy is sufficient for image capturing of the target point.
机译:操作员难以控制一个无人驾驶直升机到目的地(Masanao K.,2003);特别是在运营商和直升机之间。因为无线电控制系统在地面上机动了无人驾驶直升机。本研究的目的是使用无人直升机提高遥感跳闸控制的效率和准确性。对于本研究中使用的无人直升机,采用RTK-GPS作为定位传感器,并且在直升机中安装了提供姿势(辊子和俯仰角)的惯性传感器。此外,输出和绝对方向的地磁方向传感器(GDS)也配备了直升机,直升机安装了平板,以在机身下安装成像传感器。该跳动头可以旋转两个方向(锅和倾斜),并配备旋转编码器以测量角度。有效地改善遥感的方法是从直升机位置,姿势和目标位置计算平底锅和倾斜角度,并控制通过计算机仿真确认系统的PAN头精度。该软件还开发为支持运营商,并通过3D图形显示直升机位置和姿势。为了开发系统,我们分析了泛头瞬态和稳态响应,并建立了泛头的动态模型,并获得真正的直升机飞行数据。结果,rms误差为27.8cm,最大误差为2.69m。这种准确性足以进行目标点的图像捕获。

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