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Gyroscope‐based control and stabilization of unmanned aerial mini‐vehicle (mini‐UAV)

    Rafał Chatys Affiliation
    ; Zbigniew Koruba Affiliation

Abstract

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

Keyword : mini-UAV, mini gyroscope, strength, structure of composites

How to Cite
Chatys, R., & Koruba, Z. (2005). Gyroscope‐based control and stabilization of unmanned aerial mini‐vehicle (mini‐UAV). Aviation, 9(2), 10-16. https://doi.org/10.3846/16487788.2005.9635898
Published in Issue
Jun 30, 2005
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This work is licensed under a Creative Commons Attribution 4.0 International License.