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Motion requirements for antennas in geostationary earth orbitDesign dependencies of antennas in geostationary earth orbits are evaluated, and the tradeoffs between the optical geoscientific goals and achievable architecture capabilities are surveyed. The radial and tangential resolutions are investigated to ascertain whether mission objectives of the antennas may be satisfied. The effects of off-nadir scanning are examined to determine the limits of scan based on realizable resolution. Formulas for raster and spiral scanning time are reviewed and examined to find necessary accelerations. The resulting knowledge is used to evaluate two possible layouts. Torques necessary for slewing these configurations are calculated. A number of rotatory actuators are reviewed to evaluate future design goals for on-board momentum compensation.
Document ID
19930033932
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tentor, Lawrence B.
(NASA Langley Research Center Hampton, VA, United States)
Cudney, Harley H.
(NASA Langley Research Center Hampton, VA, United States)
Werntz, Paul
(Virginia Polytechnic Inst. and State Univ. Blacksburg, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Publication Information
Publication: In: Spaceflight mechanics 1991; Proceedings of the 1st AAS(AIAA Annual Spaceflight Mechanics Meeting, Houston, TX, Feb. 11-13, 1991. Pt. 1 (A93-17901 05-13)
Publisher: Univelt, Inc.
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AAS PAPER 91-131
Report Number: AAS PAPER 91-131
Accession Number
93A17929
Funding Number(s)
CONTRACT_GRANT: NAS1-18471
Distribution Limits
Public
Copyright
Other

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