dc.contributor.author | Sivalingam, Baheerathan | en_GB |
dc.contributor.author | Hagen, Ove Kent | en_GB |
dc.date.accessioned | 2024-04-02T08:55:35Z | |
dc.date.accessioned | 2024-11-28T10:07:56Z | |
dc.date.available | 2024-04-02T08:55:35Z | |
dc.date.available | 2024-11-28T10:07:56Z | |
dc.date.issued | 2023-10-29 | |
dc.identifier.citation | Sivalingam, Hagen. Experimentation of Monocular Visual-Aided Inertial Navigation on Fixed-Wing Unmanned Aerial Vehicle †. Engineering Proceedings. 2023;54(1) | en_GB |
dc.identifier.uri | http://hdl.handle.net/20.500.12242/3387 | |
dc.description | Sivalingam, Baheerathan; Hagen, Ove Kent.
Experimentation of Monocular Visual-Aided Inertial Navigation on Fixed-Wing Unmanned Aerial Vehicle †. Engineering Proceedings 2023 ;Volum 54.(1) | en_GB |
dc.description.abstract | This paper presents an experimental study utilizing the vision-aided inertial navigation system (VaINS) on a fixed-wing unmanned aerial vehicle (UAV). VaINS operates as a data-logging box, collecting sensor data, processing them, and transmitting the navigation solution to an operator terminal in real time. The flight data contain buildings, vegetation, a river, a lake, and mountains. The camera’s pitch angle was tested at both a grazing angle of 22° and a nadir angle of 90°. The aim of this experiment was twofold: to explore the application of VaINS on a fixed-wing UAV and to assess the performance of the image-aided navigation system. The image-aided inertial navigation system (INS) solution was compared with a reference solution during GNSS-denied time intervals. The camera’s pitch angle at 90° exhibited a slight advantage over the grazing angle at 22°. Moreover, in the linear flight segments, the image-aided navigation system demonstrated significantly better performance compared to the free inertial solution during the GNSS-denied periods. | en_GB |
dc.language.iso | en | en_GB |
dc.subject | Navigasjon | en_GB |
dc.subject | Målsøking | en_GB |
dc.title | Experimentation of Monocular Visual-Aided Inertial Navigation on Fixed-Wing Unmanned Aerial Vehicle † | en_GB |
dc.date.updated | 2024-04-02T08:55:35Z | |
dc.identifier.cristinID | 2254584 | |
dc.identifier.doi | 10.3390/ENC2023-15476 | |
dc.source.issn | 2673-4591 | |
dc.type.document | Journal article | |
dc.relation.journal | Engineering Proceedings | |