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INDES User's guide multistep input design with nonlinear rotorcraft modelingThe INDES computer program, a multistep input design program used as part of a data processing technique for rotorcraft systems identification, is described. Flight test inputs base on INDES improve the accuracy of parameter estimates. The input design algorithm, program input, and program output are presented.
Document ID
19810014193
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
November 1, 1979
Subject Category
Computer Programming And Software
Report/Patent Number
NASA-CR-159085
Report Number: NASA-CR-159085
Accession Number
81N22726
Funding Number(s)
CONTRACT_GRANT: NAS1-14549
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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