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Multi-calculation rate simulationsIt is common in real time simulations of large aerospace systems to separate the high and low frequency subsystems within the simulation and perform the integrations of the subsystems at different calculation rates. This is done to strike a balance between accuracy of calculation and capacity of the digital computer. Questions arising as to the accuracy of this structure compared to single calculation rates were studied using a linear aircraft model. Also investigated were interactions arising to cause errors worse than those expected. Problems are specifically identified and guidelines are given for selection of sample rates for multiple rate simulations.
Document ID
19780005822
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Powell, J. D.
(Stanford Univ. CA, United States)
Akhter, M.
(Stanford Univ. CA, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1977
Subject Category
Computer Programming And Software
Report/Patent Number
NASA-CR-155335
Report Number: NASA-CR-155335
Accession Number
78N13765
Funding Number(s)
CONTRACT_GRANT: NSG-2250
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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