A Linear Domain System Identification for Small Unmanned Aerial Rotorcraft Based on Adaptive Genetic Algorithm

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摘要 Thispaperproposesanewadaptivelineardomainsystemidentificationmethodforsmallunmannedaerialrotorcraft.Byusingtheflashmemoryintegratedintothemicroguidenavigationcontrolmodule,systemrecordsthedatasequencesofflighttestsasinputs(controlsignalsforservos)andoutputs(aircraft’sattitudeandvelocityinformation).Afterdatapreprocessing,thesystemconstructsthehorizontalandverticaldynamicmodelforthesmallunmannedaerialrotorcraftusingadaptivegeneticalgorithm.Theidentifiedmodelisverifiedbyaseriesofsimulationsandtests.Comparisonbetweenflightdataandtheone-steppredictiondataobtainedfromtheidentificationmodelshowsthatthedynamicmodelhasagoodestimationforrealunmannedaerialrotorcraftsystem.Basedontheproposeddynamicmodel,thesmallunmannedaerialrotorcraftcanperformhovering,turning,andstraightflighttasksinrealflighttests.
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机构地区 不详
出版日期 2010年02月12日(中国期刊网平台首次上网日期,不代表论文的发表时间)
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