Altitude and attitude control of a trirotor UAV

Ismail M. Khairuddin, Anwar P.P.A. Majeed, A. N.N. Lim, Mohd Azraai M. Razman, Abdul Aziz Jaafar

Research output: Chapter in Book or Report/Conference proceedingConference Proceedingpeer-review

Abstract

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 equipped with three fixed pitch angle rotors without the aid of a swashplate. The mathematical modelling of this multirotor is governed by the Newton-Euler formulation. A classical control algorithm viz. heuristic (Proportional-Integral-Derivative) PID tuning was adopted in the attitude and altitude control of this particular multirotor configuration. It was established from the Simulink simulations that, a PD controller was suffice to control the attitude whilst PID was apt for controlling the altitude of this form of multirotor.

Original languageEnglish
Title of host publicationManufacturing Engineering
Pages309-314
Number of pages6
DOIs
Publication statusPublished - 2014
Externally publishedYes
Event1st International Manufacturing Engineering Conference, iMEC 2013 - Gambang, Kuantan, Pahang, Malaysia
Duration: 1 Jul 20133 Jul 2013

Publication series

NameAdvanced Materials Research
Volume903
ISSN (Print)1022-6680

Conference

Conference1st International Manufacturing Engineering Conference, iMEC 2013
Country/TerritoryMalaysia
CityGambang, Kuantan, Pahang
Period1/07/133/07/13

Keywords

  • MATLAB/simulink
  • Proportional-integral-derivative (PID)
  • Trirotor
  • Unmanned aerial vehicle (UAV)
  • Vertical take-off and landing (VTOL)

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