Automated Flight Test and System Identification for Rotary Wing Small Aerial Platform Using Frequency Responses Analysis-中国期刊网

摘要 Thispaperproposesanautopilotsystemthatcanbeusedtocontrolthesmallscalerotorcraftduringtheflighttestforlinear-frequency-domainsystemidentification.Theinputfrequency-sweepisgeneratedautomaticallyaspartoftheautopilotcontrolcommand.Thereforethebandwidthcoverageandconsistencyofthefrequency-sweepareguaranteedtoproducehighqualitydataforsystemidentification.Besidethat,wecansetthesafetyparametersduringtheflighttest(maximumroll/pitchvalue,minimumaltitude,etc.)sothesafetyofthewholeflighttestisguaranteed.Thisautopilotsystemisvalidatedusinghardwareintheloopsimulatorforhoverflightcondition.

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Automated Flight Test and System Identification for Rotary Wing Small Aerial Platform Using Frequency Responses Analysis

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Automated Flight Test and System Identification for Rotary Wing Small Aerial Platform Using Frequency Responses Analysis

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