Parameter Identification of Large Spacecraft Systems, Based on the Frequency Characteristics of the Hankel Operator

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dc.contributor.advisorBaras, J.S.en_US
dc.contributor.authorAugenstain, Donald R.en_US
dc.contributor.departmentISRen_US
dc.date.accessioned2007-05-23T09:52:50Z
dc.date.available2007-05-23T09:52:50Z
dc.date.issued1992en_US
dc.description.abstractThe identification of the structural modes and damping factors of a spacecraft in orbit is accomplished. A systems approach was used to analyze the experiment and present identification techniques utilizing the frequency characteristics of the Hankel operator. Frequency domain error bounds and time domain error bounds are considered.<P>The experiment was performed on a satellite in conjunction with the Naval Research Laboratory. The experiment utilized ground based laser illumination with doppler shifted returns and identified three of the lowest vibration modes.en_US
dc.format.extent6807379 bytes
dc.format.mimetypeapplication/pdf
dc.identifier.urihttp://hdl.handle.net/1903/5332
dc.language.isoen_USen_US
dc.relation.ispartofseriesISR; MS 1992-3en_US
dc.subjectcomputer aided designen_US
dc.subjectdistributed parameter systemsen_US
dc.subjectlinear systemsen_US
dc.subjectrobust controlen_US
dc.subjectspace structuresen_US
dc.subjectsystem identificationen_US
dc.subjectSystems Integrationen_US
dc.titleParameter Identification of Large Spacecraft Systems, Based on the Frequency Characteristics of the Hankel Operatoren_US
dc.typeThesisen_US

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