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A frequency domain solution for the linear attitude-control problem of spacecraft with flexible appendagesLinear interaction problem between spacecraft attitude control and flexible appendages solved in frequency domain using Fourier transform
Document ID
19710003588
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Trubert, M. R. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 6, 2013
Publication Date
November 15, 1970
Subject Category
Navigation
Report/Patent Number
JPL-TR-32-1478
NASA-CR-111558
Report Number: JPL-TR-32-1478
Report Number: NASA-CR-111558
Accession Number
71N13063
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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