2006
DOI: 10.1007/s10846-006-9088-7
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Vision-based Target Geo-location using a Fixed-wing Miniature Air Vehicle

Abstract: This paper presents a method for determining the GPS location of a ground-based object when imaged from a fixed-wing miniature air vehicle (MAV). Using the pixel location of the target in an image, with measurements of MAV position and attitude, and camera pose angles, the target is localized in world coordinates. The main contribution of this paper is to present four techniques for reducing the localization error. In particular, we discuss RLS filtering, bias estimation, flight path selection, and wind estima… Show more

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Cited by 188 publications
(104 citation statements)
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References 16 publications
(21 reference statements)
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“…광학카메라 기반의 목표물 위치 추정 [3] 광학 카메라 기반의 목표물 위치 추정은 영상 정보 내에 서 목표물의 픽셀위치를 알고 있다는 가정을 바탕으로 한 그림4. 지상목표물(마커) 항공촬영및짐벌트래킹.…”
Section: 위치 추정 알고리즘unclassified
“…광학카메라 기반의 목표물 위치 추정 [3] 광학 카메라 기반의 목표물 위치 추정은 영상 정보 내에 서 목표물의 픽셀위치를 알고 있다는 가정을 바탕으로 한 그림4. 지상목표물(마커) 항공촬영및짐벌트래킹.…”
Section: 위치 추정 알고리즘unclassified
“…In order to illustrate the effectiveness of the modified guidance law, a simulation is conducted in which the bang-bang controller proposed in [10], as shown in Eq. (20), was used:…”
Section:  mentioning
confidence: 99%
“…For stationary target tracking, circular trajectories overhead the target are widely accepted in the literature as good trajectories. 5,38,46 However, the optimal circling radius is not known and, if the target is moving, the operator may not deduce the best vehicle trajectory. Autonomous flight path generation is therefore essential to successful target localization.…”
Section: Ia Motivationmentioning
confidence: 99%
“…Ivey and Johnson 18 propose a vision-based target tracking filter for use on board a UAV, comparing both an Extended Kalman Filter (EKF) and a Square-Root Unscented Kalman Filter (SRUKF). Barber et al 5 explore stationary target localization from small fixed-wing UAVs using a Recursive Least Squares (RLS) filter. They also explore flight path optimization by finding an optimal altitude and radius for a circular trajectory above the stationary target.…”
mentioning
confidence: 99%