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Rectification errors of a strapdown single axis platform under vibration inputs.Rectification errors of strapdown single axis platform spacecraft guidance system under structural vibration inputs, using digital computer prediction methods
Document ID
19680056558
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rountree, R. C.
Date Acquired
August 4, 2013
Publication Date
August 1, 1968
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Navigation
Report/Patent Number
AIAA PAPER 68-827
Report Number: AIAA PAPER 68-827
Meeting Information
Meeting: GUIDANCE, CONTROL, AND FLIGHT DYNAMICS CONFERENCE
Location: PASADENA, CA
Start Date: August 12, 1968
End Date: August 14, 1968
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
68A37530
Funding Number(s)
CONTRACT_GRANT: NAS8-20209
Distribution Limits
Public
Copyright
Other

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