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...

Full description

Bibliographic Details
Main Authors: Rafał Chatys, Zbigniew Koruba
Format: Article
Language:English
Published: Vilnius Gediminas Technical University 2005-06-01
Series:Aviation
Subjects:
Online Access:https://journals.vgtu.lt/index.php/Aviation/article/view/7410
_version_ 1819291205971738624
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