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MAV control system design based on virtual instrument

  • Beihang University

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

Abstract

A new design scheme of micro Rotorcraft Unmanned Aerial Vehicle (MRUAV) control system based on Virtual Instrument (VI) is developed in this paper. The control platform constructed by NI CompactRIO (a VI device) is used to realize the flight data acquisition, control algorithm design and control command transmission instead of the conventional flight controller. Considering the inaccuracy of the mathematical model and the adverse influence of high-frequency vibration, the Active Disturbance Rejection Controller (ADRC) not relying on the accurate mathematical model of controlled plant is selected as the control algorithm. The suitable ADRC parameters are recognized through successive approximation with the help of the online debugging function of VI. Finally, Flight experiments show the validity of the control system.

Original languageEnglish
Title of host publication2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages474-479
Number of pages6
ISBN (Electronic)9781479946990
DOIs
StatePublished - 12 Jan 2015
Event6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 - Yantai, China
Duration: 8 Aug 201410 Aug 2014

Publication series

Name2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

Conference

Conference6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
Country/TerritoryChina
CityYantai
Period8/08/1410/08/14

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