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Rapid GNSS-based calibration and target localization strategy for deployable optical UAV detection systems
Author(s) -
Christopher Naverschnigg,
Andreas Sinn,
Konstantin Waltenberger,
Denis Ojdanic,
Georg Schitter
Publication year - 2025
Publication title -
ieee sensors journal
Language(s) - English
Resource type - Magazines
SCImago Journal Rank - 0.681
H-Index - 121
eISSN - 1558-1748
pISSN - 1530-437X
DOI - 10.1109/jsen.2025.3594402
Subject(s) - signal processing and analysis , communication, networking and broadcast technologies , components, circuits, devices and systems , robotics and control systems
This paper presents the design and experimental evaluation of the feasibility of a rapid Global Navigation Satellite System (GNSS)-based calibration and target localization strategy within a process structure for deployable optical UAV detection systems in combination with complementary sensors, such as radar. The calibration strategy utilizes a cooperative UAV with standard GNSS point positioning to determine unknown orientation parameters of a deployable telescope-based system within a global reference system. During a calibration flight, the cooperative UAV with a GNSS receiver is automatically tracked using a deep-learning-based detector and a pan/tilt mount. By combining flight log data of the UAV, detector and mount data, orientation parameters of the system relative to the World Geodetic System 1984 are determined. Uncertainties of internal and external sources are investigated and the proposed process structure is enhanced by a target localization strategy based on Lissajous search trajectories, which is also validated during field tests in combination with a radar system after applying the proposed calibration procedure. During field tests, a remaining angular calibration root mean square (RMS) error of 0.255° in elevation and 0.277° in azimuth is achieved using a DJI Mini 2 and a calibration flight duration of 100 s. By locating and tracking a validation UAV, an RMS error of 0.376° in elevation and 0.336° in azimuth is achieved.

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