DocumentCode :
2871709
Title :
Model predictive attitude control of vario unmanned helicopter
Author :
Samal, Mahendra Kumar ; Garratt, Matthew ; Pota, Hemanshu ; Sangani, Hamid Teimoori
Author_Institution :
Sch. of Eng. & Inf. Technol., Univ. of New South Wales at ADFA, Canberra, ACT, Australia
fYear :
2011
fDate :
7-10 Nov. 2011
Firstpage :
622
Lastpage :
627
Abstract :
This paper presents a Model Predictive Control (MPC) based attitude stabilisation system for a rotary-wing unmanned aerial vehicle. We have enhanced the MPC performance by augmenting the helicopter model with servo dynamics during the prediction phase. The inclusion of servo dynamics and time delay yields a smoother control response. A linear state space reduced order model for longitudinal and lateral dynamics of the helicopter is used for controller design. The applicability of the proposed MPC scheme is evaluated on a nonlinear simulation model of an unmanned helicopter for autonomous hover and low speed forward flight. Numerical simulation on the nonlinear model illustrates improved performance of the closed-loop system in presence of servo dynamics and time delays.
Keywords :
attitude control; autonomous aerial vehicles; closed loop systems; control system synthesis; delays; helicopters; mobile robots; predictive control; MPC; Vario unmanned helicopter; attitude stabilisation system; closed-loop system; controller design; linear state space; model predictive attitude control; nonlinear simulation model; prediction phase; rotary wing unmanned aerial vehicle; servo dynamics; time delays; Actuators; Aerodynamics; Computational modeling; Delay effects; Helicopters; Predictive models; Servomotors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
IECON 2011 - 37th Annual Conference on IEEE Industrial Electronics Society
Conference_Location :
Melbourne, VIC
ISSN :
1553-572X
Print_ISBN :
978-1-61284-969-0
Type :
conf
DOI :
10.1109/IECON.2011.6119382
Filename :
6119382
Link To Document :
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