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GOES-R Series GEO Side-Lobe Capable GPSR Post-Launch Refinements and Operational CapabilitiesThis paper addresses three topics: 1) EOPP (EOP (Earth Orientation Prediction) Parameters) file modification, 2) Kalman filter parameter tuning regarding maneuvers and 3) off-pointing GPS (Global Positioning System) tracking capability. GOES-R (Geostationary Operational Environmental Satellite-R Series) is the first in a 4-part series of new weather satellites set to replace and upgrade the older GOES constellation. Two GOES-R series have been launched to date, GOES-S and GOES-R. GOES-R is operational over the Eastern United States and GOES-S over the West. The Global Positioning System Receiver (GPSR) on board this geostationary weather satellite is a mission critical enabling technology which has been both tested on the ground and evaluated on-orbit to verify its effectivity. Since becoming operational in November 2016, the GPSR onboard has performed extremely well under nominal circumstances. Further refinements regarding a variety of facets have taken place since the launch of GOES-R. One such refinement was the implementation of a modified EOP (Earth Orientation Prediction) parameter set to improve ECEF (Earth Centered Earth Fixed) to ECI (Earth Centered Inertial) transformation by restoring zonal tides removed from the EOP parameter fit per tech note 36. Another relevant refinement combined thermal consideration with Kalman filter tuning to improve orbit determination performance during maneuvers. Now with two years of data and two vehicles in orbit many capabilities of the GPSR have been identified and defined to a higher degree. For example, metrics on side-lobe tracking and off-Nadir tracking capabilities have been quantified to a high degree. This paper will seek to supplement the ESA (European Space Agency) GNC 2017 GOES-R GPSR performance paper as a deeper dive on specific tracking capabilities and performance improvements now implemented on the GOES-R and GOES-S vehicles.
Document ID
20190002515
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Ramsey, Graeme
(Lockheed Martin Space Systems Co. Denver, CO, United States)
Barker, Lee
(Lockheed Martin Space Systems Co. Denver, CO, United States)
Chapel, Jim
(Lockheed Martin Space Systems Co. Denver, CO, United States)
Winkler, Stephen
(Lockheed Martin Space Systems Co. Denver, CO, United States)
Frey, Chuck
(Lockheed Martin Space Systems Co. King of Prussia, PA, United States)
Freesland, Douglas
(ACS Engineering Corp. Greenbelt, MD, United States)
Baltimore, Perry
(Arctic Slope Technical Services, Inc. Beltsville, MD, United States)
Krimchansky, Alexander
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
April 17, 2019
Publication Date
February 1, 2019
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
GSFC-E-DAA-TN65667
AAS 19-074
Meeting Information
Meeting: American Astronautical Society Annual Guidance and Control Conference (AAS GNC 2019)
Location: Breckenridge, CO
Country: United States
Start Date: February 1, 2019
End Date: February 6, 2019
Sponsors: American Astronautical Society
Funding Number(s)
CONTRACT_GRANT: NNG09HR00C
CONTRACT_GRANT: NNG15CR65C
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Keywords
GPS Receiver
GOES-R
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