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Solar Radiation Pressure Binning for the Geosynchronous OrbitOrbital maintenance parameters for individual satellites or groups of satellites have traditionally been set by examining orbital parameters alone, such as through apogee and perigee height binning; this approach ignored the other factors that governed an individual satellite's susceptibility to non-conservative forces. In the atmospheric drag regime, this problem has been addressed by the introduction of the "energy dissipation rate," a quantity that represents the amount of energy being removed from the orbit; such an approach is able to consider both atmospheric density and satellite frontal area characteristics and thus serve as a mechanism for binning satellites of similar behavior. The geo-synchronous orbit (of broader definition than the geostationary orbit -- here taken to be from 1300 to 1800 minutes in orbital period) is not affected by drag; rather, its principal non-conservative force is that of solar radiation pressure -- the momentum imparted to the satellite by solar radiometric energy. While this perturbation is solved for as part of the orbit determination update, no binning or division scheme, analogous to the drag regime, has been developed for the geo-synchronous orbit. The present analysis has begun such an effort by examining the behavior of geosynchronous rocket bodies and non-stabilized payloads as a function of solar radiation pressure susceptibility. A preliminary examination of binning techniques used in the drag regime gives initial guidance regarding the criteria for useful bin divisions. Applying these criteria to the object type, solar radiation pressure, and resultant state vector accuracy for the analyzed dataset, a single division of "large" satellites into two bins for the purposes of setting related sensor tasking and orbit determination (OD) controls is suggested. When an accompanying analysis of high area-to-mass objects is complete, a full set of binning recommendations for the geosynchronous orbit will be available.
Document ID
20110015238
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Hejduk, M. D.
(AI Solutions, Inc. Lanham, MD, United States)
Ghrist, R. W.
(AI Solutions, Inc. Lanham, MD, United States)
Date Acquired
August 25, 2013
Publication Date
July 31, 2011
Subject Category
Astrodynamics
Report/Patent Number
GSFC.CP.4921.2011
AAS 11-581
Report Number: GSFC.CP.4921.2011
Report Number: AAS 11-581
Meeting Information
Meeting: 2011 AIAA/AAS Astrodynamics Specialist Conference
Location: Girdwood, AK
Country: United States
Start Date: July 31, 2011
End Date: August 3, 2011
Sponsors: American Astronautical Society, American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNG10CP02C
Distribution Limits
Public
Copyright
Public Use Permitted.
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