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    Predicting the Optical Performance of the Space Interferometry Mission Using a Modeling, Testing, and Validation Methodology

    Source: Journal of Vibration and Acoustics:;2007:;volume( 129 ):;issue: 002::page 148
    Author:
    Ipek Basdogan
    ,
    Laila Mireille Elias
    ,
    Frank Dekens
    ,
    Lisa Sievers
    DOI: 10.1115/1.2202152
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the modeling, testing, and validation methodologies developed to predict the optical performance of the Space Interferometry Mission (SIM) at the Jet Propulsion Laboratory (JPL). The modeling methodology combines structural, optical, and control system design within a common state space framework and incorporates reaction wheel assembly (RWA) disturbances to evaluate the end-to-end performance of the system requirements. The validation methodology uses the Micro-Precision Interferometer (MPI) testbed, which is a ground-based, representative hardware model of SIM. In this study, the integrated model of the MPI testbed was used to calculate the transfer functions from RWA input to optical performance output. The model-predicted transfer functions were compared with the MPI testbed measurements, and the accuracy of the integrated model was quantified using a metric that was based on output power of the transfer functions. The RWA disturbances were then propagated through the modeled and measured transfer functions to predict the optical performance of the MPI testbed. This method is called the “decoupled disturbance analysis” and relies on the “blocked” RWA disturbances, measured with the RWA hardmounted to a rigid surface. These predictions were compared with the actual (measured) optical performance of MPI, measured with the RWA mounted to MPI, to evaluate the accuracy of the decoupled disturbance analysis method. The results show that this method is not an accurate representation of the coupled boundary conditions that occurs when the RWA is mounted to the flexible MPI structure. In order to correct for the blocked RWA disturbance boundary conditions, the “coupled disturbance analysis” method was developed. This method uses “force filters” that depend on estimates of the interface accelerances of the RWA and the MPI structure to effectively transform the blocked RWA disturbance measurements into their corresponding “coupled” disturbances (the disturbances that would occur at the coupled RWA-MPI interface). Compared to the decoupled method, the coupled method more accurately predicts the system’s performance. Additionally, the RWA cross-spectral density terms were found to be influential in matching the performance predictions to the measured optical performance of MPI.
    keyword(s): Interferometry , Interferometers , Transfer functions , Modeling , Testing , Force , Filters , Wheels , Measurement , Accuracy AND Boundary-value problems ,
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      Predicting the Optical Performance of the Space Interferometry Mission Using a Modeling, Testing, and Validation Methodology

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/137149
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    • Journal of Vibration and Acoustics

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    contributor authorIpek Basdogan
    contributor authorLaila Mireille Elias
    contributor authorFrank Dekens
    contributor authorLisa Sievers
    date accessioned2017-05-09T00:26:24Z
    date available2017-05-09T00:26:24Z
    date copyrightApril, 2007
    date issued2007
    identifier issn1048-9002
    identifier otherJVACEK-28885#148_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/137149
    description abstractThis paper presents the modeling, testing, and validation methodologies developed to predict the optical performance of the Space Interferometry Mission (SIM) at the Jet Propulsion Laboratory (JPL). The modeling methodology combines structural, optical, and control system design within a common state space framework and incorporates reaction wheel assembly (RWA) disturbances to evaluate the end-to-end performance of the system requirements. The validation methodology uses the Micro-Precision Interferometer (MPI) testbed, which is a ground-based, representative hardware model of SIM. In this study, the integrated model of the MPI testbed was used to calculate the transfer functions from RWA input to optical performance output. The model-predicted transfer functions were compared with the MPI testbed measurements, and the accuracy of the integrated model was quantified using a metric that was based on output power of the transfer functions. The RWA disturbances were then propagated through the modeled and measured transfer functions to predict the optical performance of the MPI testbed. This method is called the “decoupled disturbance analysis” and relies on the “blocked” RWA disturbances, measured with the RWA hardmounted to a rigid surface. These predictions were compared with the actual (measured) optical performance of MPI, measured with the RWA mounted to MPI, to evaluate the accuracy of the decoupled disturbance analysis method. The results show that this method is not an accurate representation of the coupled boundary conditions that occurs when the RWA is mounted to the flexible MPI structure. In order to correct for the blocked RWA disturbance boundary conditions, the “coupled disturbance analysis” method was developed. This method uses “force filters” that depend on estimates of the interface accelerances of the RWA and the MPI structure to effectively transform the blocked RWA disturbance measurements into their corresponding “coupled” disturbances (the disturbances that would occur at the coupled RWA-MPI interface). Compared to the decoupled method, the coupled method more accurately predicts the system’s performance. Additionally, the RWA cross-spectral density terms were found to be influential in matching the performance predictions to the measured optical performance of MPI.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePredicting the Optical Performance of the Space Interferometry Mission Using a Modeling, Testing, and Validation Methodology
    typeJournal Paper
    journal volume129
    journal issue2
    journal titleJournal of Vibration and Acoustics
    identifier doi10.1115/1.2202152
    journal fristpage148
    journal lastpage157
    identifier eissn1528-8927
    keywordsInterferometry
    keywordsInterferometers
    keywordsTransfer functions
    keywordsModeling
    keywordsTesting
    keywordsForce
    keywordsFilters
    keywordsWheels
    keywordsMeasurement
    keywordsAccuracy AND Boundary-value problems
    treeJournal of Vibration and Acoustics:;2007:;volume( 129 ):;issue: 002
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian