Real-time wind estimation on a micro unmanned aerial vehicle using its inertial measurement unit

被引:120
|
作者
Neumann, Patrick P. [1 ]
Bartholmai, Matthias [1 ]
机构
[1] BAM Fed Inst Mat Res & Testing, D-12205 Berlin, Germany
关键词
Micro unmanned aerial vehicle (UAV); Quadrocopter; Real-time; Inertial measurement unit (IMU); Airspeed calibration; Wind estimation (speed and direction);
D O I
10.1016/j.sna.2015.09.036
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
This paper presents an approach for a quadrocoper-based micro unmanned aerial vehicle (UAV) that estimates the wind vector (speed and direction) in real-time based on measurement data of its on-board sensors only. This method does not need any additional airspeed sensor or dedicated anemometer, and thus the micro UAV's valuable payload remains free for other sensors. Wind tunnel and field tests were used to evaluate the performance of the approach. In order to quantify its accuracy, experiments are presented where data was collected with an anemometer placed in an open field with the micro UAV in flight following a predefined trajectory around the anemometer and hovering at a defined position close to it. (C) 2015 Elsevier B.V. All rights reserved.
引用
收藏
页码:300 / 310
页数:11
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