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Dynamic Response Tests Of Inertial And Optical Wind Tunnel Model Attitude Measurement Devices
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722186227 Total Pages :46 pages Book Rating :4.1/5 (862 download)
Book Synopsis Dynamic Response Tests of Inertial and Optical Wind-Tunnel Model Attitude Measurement Devices by : National Aeronautics and Space Administration (NASA)
Download or read book Dynamic Response Tests of Inertial and Optical Wind-Tunnel Model Attitude Measurement Devices written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-02 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results are presented for an experimental study of the response of inertial and optical wind-tunnel model attitude measurement systems in a wind-off simulated dynamic environment. This study is part of an ongoing activity at the NASA Langley Research Center to develop high accuracy, advanced model attitude measurement systems that can be used in a dynamic wind-tunnel environment. This activity was prompted by the inertial model attitude sensor response observed during high levels of model vibration which results in a model attitude measurement bias error. Significant bias errors in model attitude measurement were found for the measurement using the inertial device during wind-off dynamic testing of a model system. The amount of bias present during wind-tunnel tests will depend on the amplitudes of the model dynamic response and the modal characteristics of the model system. Correction models are presented that predict the vibration-induced bias errors to a high degree of accuracy for the vibration modes characterized in the simulated dynamic environment. The optical system results were uncorrupted by model vibration in the laboratory setup. Buehrle, R. D. and Young, C. P., Jr. and Burner, A. W. and Tripp, J. S. and Tcheng, P. and Finley, T. D. and Popernack, T. G., Jr. Langley Research Center RTOP 505-59-54-01...
Book Synopsis Dynamic Response Tests of Inertial and Optical Wind-tunnel Model Attitude Measurement Devices by :
Download or read book Dynamic Response Tests of Inertial and Optical Wind-tunnel Model Attitude Measurement Devices written by and published by . This book was released on 1995 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722196233 Total Pages :36 pages Book Rating :4.1/5 (962 download)
Book Synopsis Effects of Vibration on Inertial Wind-Tunnel Model Attitude Measurement Devices by : National Aeronautics and Space Administration (NASA)
Download or read book Effects of Vibration on Inertial Wind-Tunnel Model Attitude Measurement Devices written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-02 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results of an experimental study of a wind tunnel model inertial angle-of-attack sensor response to a simulated dynamic environment are presented. The inertial device cannot distinguish between the gravity vector and the centrifugal accelerations associated with wind tunnel model vibration, this situation results in a model attitude measurement bias error. Significant bias error in model attitude measurement was found for the model system tested. The model attitude bias error was found to be vibration mode and amplitude dependent. A first order correction model was developed and used for estimating attitude measurement bias error due to dynamic motion. A method for correcting the output of the model attitude inertial sensor in the presence of model dynamics during on-line wind tunnel operation is proposed. Young, Clarence P., Jr. and Buehrle, Ralph D. and Balakrishna, S. and Kilgore, W. Allen Langley Research Center RTOP 505-59-54-01...
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Book Synopsis Effects of Vibration on Inertial Wind-tunnel Model Attitude Measurement Devices by :
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Book Synopsis Effects of Vibration on Inertial Wind-tunnel Model Attitude Measurement Devices by : Clarence P. Young
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