Altitude and Attitude Control of a Trirotor UAV

This paper outlines the dynamic modelling as well as the attitude and altitude control of a rotary based unmanned aerial vehicle (UAV). A multirotor vertical take-off and landing (VTOL) UAVs, namely Trirotor aircraft is investigated. In essence the the trirotor model consists of three DC motors equi...

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Bibliographic Details

Main Authors:	Ismail, Mohd Khairuddin, Anwar, P. P. Abdul Majeed, Ann, Lim, Mohd Azraai, M. Razman, Abdul Aziz, Jaafar
Format:	Article
Published:	Trans Tech Publications, Switzerland 2014
Subjects:	TS Manufactures
Online Access:	http://umpir.ump.edu.my/id/eprint/5542/ http://dx.doi.org/10.4028/www.scientific.net/AMR.903.309
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