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Compensation based on linearized analysis for a six degree of freedom motion simulatorThe inertial response characteristics of a synergistic, six-degree-of-freedom motion base are presented in terms of amplitude ratio and phase lag as functions of frequency data for the frequency range of interest (0 to 2 Hz) in real time, digital, flight simulators. The notch filters which smooth the digital-drive signals to continuous drive signals are presented, and appropriate compensation, based on the inertial response data, is suggested. The existence of an inverse transformation that converts actuator extensions into inertial positions makes it possible to gather the response data in the inertial axis system.
Document ID
19740002188
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Parrish, R. V.
(NASA Langley Research Center Hampton, VA, United States)
Dieudonne, J. E.
(NASA Langley Research Center Hampton, VA, United States)
Martin, D. J., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Copeland, J. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1973
Subject Category
Facilities, Research, And Support
Report/Patent Number
L-9023
NASA-TN-D-7349
Report Number: L-9023
Report Number: NASA-TN-D-7349
Accession Number
74N10301
Funding Number(s)
PROJECT: RTOP 501-39-11-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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