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Development of an autonomous control system for a small fixed pitch helicopter

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conference contribution
posted on 24.11.2010, 17:25 authored by Owen McAree, Jonathan H.A. Clarke, Wen-Hua ChenWen-Hua Chen
The indoor test bed of the Autonomous Systems Laboratory has been used to create a control system for a small fixed pitch helicopter. This paper outlines the challenges posed by such a vehicle and the control system designed to overcome them. The control system utilized a visual tracking system to obtain state information without onboard hardware. Matlab/Simulink environment was used to facilitate rapid prototyping control development. An autopilot consisting of multi-channel PID controllers was implemented for flight tests. Failsafe strategies and gain scheduling were both investigated and implemented with the use of a graphical user interface. A number of flight tests were conducted and the results are provided. The future work of the laboratory is also covered.

History

School

  • Aeronautical, Automotive, Chemical and Materials Engineering

Department

  • Aeronautical and Automotive Engineering

Citation

MCAREE, O., CLARKE, J. and CHEN, W.-H., 2010. Development of an autonomous control system for a small fixed pitch helicopter. IN: 2nd International Conference on Advanced Computer Control (ICACC), Shenyang, 27-29 March, pp. 13 - 17

Publisher

© IEEE

Version

VoR (Version of Record)

Publication date

2010

Notes

This is a conference paper [©IEEE]. Personal use of this material is permitted. However, permission to reprint/republish this material for advertising or promotional purposes or for creating new collective works for resale or redistribution to servers or lists, or to reuse any copyrighted component of this work in other works must be obtained from the IEEE.

ISBN

9781424458455

Language

en

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