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An approximate solution to improve computational efficiency of impedance-type payload load predictionThe computational efficiency of the impedance type loads prediction method was studied. Three goals were addressed: devise a method to make the impedance method operate more efficiently in the computer; assess the accuracy and convenience of the method for determining the effect of design changes; and investigate the use of the method to identify design changes for reduction of payload loads. The method is suitable for calculation of dynamic response in either the frequency or time domain. It is concluded that: the choice of an orthogonal coordinate system will allow the impedance method to operate more efficiently in the computer; the approximate mode impedance technique is adequate for determining the effect of design changes, and is applicable for both statically determinate and statically indeterminate payload attachments; and beneficial design changes to reduce payload loads can be identified by the combined application of impedance techniques and energy distribution review techniques.
Document ID
19810018652
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
White, C. W.
(Martin Marietta Corp. Denver, CO, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1981
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-165719
MRC-80-654
Report Number: NASA-CR-165719
Report Number: MRC-80-654
Accession Number
81N27190
Funding Number(s)
CONTRACT_GRANT: NAS1-14370
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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