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

Autor:	Rafał Chatys, Zbigniew Koruba
Jazyk:	angličtina
Rok vydání:	2005
Předmět:	mini-UAV mini gyroscope strength structure of composites Motor vehicles. Aeronautics. Astronautics TL1-4050
Zdroj:	Aviation, Vol 9, Iss 2 (2005)
Druh dokumentu:	article
ISSN:	16487788 1648-7788 1822-4180
DOI:	10.3846/16487788.2005.9635898
Popis:	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
Databáze:	Directory of Open Access Journals
Externí odkaz:	https://doaj.org/article/c491b578abf2467891115d971dd00a65 Zobrazit plný text záznamu View record in DOAJ Plný text ve formátu PDF