Gyroscope‐based control and stabilization of unmanned aerial mini‐vehicle (mini‐UAV)
This work discusses the use of a mini gyroscope with three degrees of freedom to control or remote control an unmanned aerial mini‐vehicle (mini‐UAV). The gyroscope determines the reference system for the navigation of the UAV. The algorithm of the gyroscope control moments and the law of deflection...
Main Authors: | , |
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Format: | Article |
Language: | English |
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Vilnius Gediminas Technical University
2005-06-01
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Series: | Aviation |
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Online Access: | https://journals.vgtu.lt/index.php/Aviation/article/view/7410 |
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author | Rafał Chatys Zbigniew Koruba |
author_facet | Rafał Chatys Zbigniew Koruba |
author_sort | Rafał Chatys |
collection | DOAJ |
description | This work discusses the use of a mini gyroscope with three degrees of freedom to control or remote control an unmanned aerial mini‐vehicle (mini‐UAV). The gyroscope determines the reference system for the navigation of the UAV. The algorithm of the gyroscope control moments and the law of deflection of the UAV surface control are presented. The mini autopilot plays a role of a system that makes the longitudinal line coincide with the gyroscope axis. The structure and durability aspects of the remote and programmed navigation are considered.
First Published Online: 14 Oct 2010 |
first_indexed | 2024-12-24T03:34:57Z |
format | Article |
id | doaj.art-c491b578abf2467891115d971dd00a65 |
institution | Directory Open Access Journal |
issn | 1648-7788 1822-4180 |
language | English |
last_indexed | 2024-12-24T03:34:57Z |
publishDate | 2005-06-01 |
publisher | Vilnius Gediminas Technical University |
record_format | Article |
series | Aviation |
spelling | doaj.art-c491b578abf2467891115d971dd00a652022-12-21T17:17:06ZengVilnius Gediminas Technical UniversityAviation1648-77881822-41802005-06-019210.3846/16487788.2005.9635898Gyroscope‐based control and stabilization of unmanned aerial mini‐vehicle (mini‐UAV)Rafał Chatys0Zbigniew Koruba1Kielce University of Technology (KUT), Al.1000-lecia P.P. 7, 25-314, PolandKielce University of Technology (KUT), Al.1000-lecia P.P. 7, 25-314, PolandThis work discusses the use of a mini gyroscope with three degrees of freedom to control or remote control an unmanned aerial mini‐vehicle (mini‐UAV). The gyroscope determines the reference system for the navigation of the UAV. The algorithm of the gyroscope control moments and the law of deflection of the UAV surface control are presented. The mini autopilot plays a role of a system that makes the longitudinal line coincide with the gyroscope axis. The structure and durability aspects of the remote and programmed navigation are considered. First Published Online: 14 Oct 2010https://journals.vgtu.lt/index.php/Aviation/article/view/7410mini-UAVmini gyroscopestrengthstructure of composites |
spellingShingle | Rafał Chatys Zbigniew Koruba Gyroscope‐based control and stabilization of unmanned aerial mini‐vehicle (mini‐UAV) Aviation mini-UAV mini gyroscope strength structure of composites |
title | Gyroscope‐based control and stabilization of unmanned aerial mini‐vehicle (mini‐UAV) |
title_full | Gyroscope‐based control and stabilization of unmanned aerial mini‐vehicle (mini‐UAV) |
title_fullStr | Gyroscope‐based control and stabilization of unmanned aerial mini‐vehicle (mini‐UAV) |
title_full_unstemmed | Gyroscope‐based control and stabilization of unmanned aerial mini‐vehicle (mini‐UAV) |
title_short | Gyroscope‐based control and stabilization of unmanned aerial mini‐vehicle (mini‐UAV) |
title_sort | gyroscope based control and stabilization of unmanned aerial mini vehicle mini uav |
topic | mini-UAV mini gyroscope strength structure of composites |
url | https://journals.vgtu.lt/index.php/Aviation/article/view/7410 |
work_keys_str_mv | AT rafałchatys gyroscopebasedcontrolandstabilizationofunmannedaerialminivehicleminiuav AT zbigniewkoruba gyroscopebasedcontrolandstabilizationofunmannedaerialminivehicleminiuav |