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Implementation of a semi-active gravity gradient controller.Semiactive gravity gradient stabilization system design for low altitude earth oriented spacecraft attitude control, using active reaction wheel scanner
Document ID
19690040345
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hui, P. S.
Zaremba, J. G.
Date Acquired
August 5, 2013
Publication Date
December 1, 1968
Subject Category
Space Vehicles
Meeting Information
Meeting: U.S. AIR FORCE SYSTEMS COMMAND AND AEROSPACE CORP., SYMPOSIUM ON GRAVITY GRADIENT ATTITUDE STABILIZATION
Location: EL SEGUNDO, CALIF.
Start Date: December 3, 1968
End Date: December 5, 1968
Sponsors: U.S. AIR FORCE SYSTEMS COMMAND AND AEROSPACE CORP.
Accession Number
69A18334
Funding Number(s)
CONTRACT_GRANT: NAS5-10253
CONTRACT_GRANT: NAS5-10453
Distribution Limits
Public
Copyright
Other

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