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Design approach for reducing gyro-induced errors in strapdown inertial systems.Single degree of freedom integrating gyro in strapdown inertial systems, discussing error reduction
Document ID
19680056561
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gelb, A.
Sutherland, A. A., Jr.
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 68-830
Report Number: AIAA PAPER 68-830
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
68A37533
Funding Number(s)
CONTRACT_GRANT: NAS12-508
Distribution Limits
Public
Copyright
Other

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