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Development of a nonlinear 6-degree of freedom miniature rotary-wing unmanned aerial vehicle software model and PID flight path controller using Mathworks Simulink simulation environment

Thesis (M.S. in Electrical Engineering)--Naval Postgraduate School, September 2009. / Thesis Advisor(s): Hutchins, Robert G. ; Dobrokhodov, Vladimir ; Kitsios, Ioannis. "September 2009." Description based on title screen as viewed on November 5, 2009. Author(s) subject terms: Hardware in the Loop (HIL), Software in the Loop (SIL) Simulation Environment, 6-Degree of Freedom (6-DOF) Rotary-wing Unmanned Aerial Vehicle (RW UAV) model , PID Flight Path Controllers Includes bibliographical references (p. 111). Also available in print.

Identiferoai:union.ndltd.org:OCLC/oai:xtcat.oclc.org:OCLCNo/463643495
Date January 2009
CreatorsMiranda, Ricardo E.
PublisherMonterey, California : Naval Postgraduate School,
Source SetsOCLC
LanguageEnglish
Detected LanguageEnglish
Source(2 MB)

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