摘要
Thispaperproposesanewadaptivelineardomainsystemidentificationmethodforsmallunmannedaerialrotorcraft.Byusingtheflashmemoryintegratedintothemicroguidenavigationcontrolmodule,systemrecordsthedatasequencesofflighttestsasinputs(controlsignalsforservos)andoutputs(aircraft’sattitudeandvelocityinformation).Afterdatapreprocessing,thesystemconstructsthehorizontalandverticaldynamicmodelforthesmallunmannedaerialrotorcraftusingadaptivegeneticalgorithm.Theidentifiedmodelisverifiedbyaseriesofsimulationsandtests.Comparisonbetweenflightdataandtheone-steppredictiondataobtainedfromtheidentificationmodelshowsthatthedynamicmodelhasagoodestimationforrealunmannedaerialrotorcraftsystem.Basedontheproposeddynamicmodel,thesmallunmannedaerialrotorcraftcanperformhovering,turning,andstraightflighttasksinrealflighttests.
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)