Worst-case GPS constellation for testing navigation at geosynchronous orbit for GOES-R

Kristin Larson, David Gaylor, Stephen Winkler

Research output: Chapter in Book/Report/Conference proceedingConference contribution

3 Citations (Scopus)

Abstract

The Geostationary Operational Environmental Satellite - R Series (GOES-R) is the next generation NOAA weather satellite to be launched in 2015. GOES-R will use an L1 C/A GPS receiver (GPSR) to receive both GPS main beam and side lobe signals. The quality and availability of GPS signals at geosynchronous orbit (GEO) strongly impact navigation accuracy. For the GOES-R program, navigation accuracy requirements must be maintained during nominal operation of the spacecraft including station-keeping maneuvers. The GPSR solution 3-sigma accuracy requirement in position knowledge is 75 meters for the in-track and cross-track directions, and 100 meters for radial direction. Since maneuvers are not modeled in the onboard GPSR software, accuracy can degrade significantly during a maneuver. In order to verify that the GOES-R GPS navigation system can meet the stringent accuracy requirements during station- keeping maneuvers, a worst-case test scenario was developed for receiver testing. To find this scenario, we developed a simulation that models the GPS constellation and a GPS receiver and determines whether each GPS space vehicle (SV) can be tracked based on a high fidelity link budget model. Using this simulation, we modified the position of the GPS constellation relative to the Earth to find the scenario with the fewest number of trackable SVs during a North-South stationkeeping maneuver. The lowest visibility cases were found to be dependent on the right ascension, and occurred at 6 different shifts in right ascension. GPS receiver results from the Engineering Development Unit (EDU) are provided for both nominal and worst-case performance.

Original languageEnglish (US)
Title of host publicationAdvances in the Astronautical Sciences
PublisherUnivelt Inc.
Pages403-416
Number of pages14
Volume149
StatePublished - 2013
Externally publishedYes
Event2013 36th Annual AAS Rocky Mountain Section Guidance and Control Conference, Guidance and Control 2013 - Breckenridge, CO, United States
Duration: Feb 1 2013Feb 6 2013

Other

Other2013 36th Annual AAS Rocky Mountain Section Guidance and Control Conference, Guidance and Control 2013
CountryUnited States
CityBreckenridge, CO
Period2/1/132/6/13

Fingerprint

geosynchronous orbits
constellations
GOES
navigation
maneuvers
Global positioning system
Navigation
Orbits
GPS
receivers
Satellites
Testing
requirements
spacecraft
stationkeeping
stations
low visibility
product development
weather
lobes

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

Cite this

Larson, K., Gaylor, D., & Winkler, S. (2013). Worst-case GPS constellation for testing navigation at geosynchronous orbit for GOES-R. In Advances in the Astronautical Sciences (Vol. 149, pp. 403-416). Univelt Inc..

Worst-case GPS constellation for testing navigation at geosynchronous orbit for GOES-R. / Larson, Kristin; Gaylor, David; Winkler, Stephen.

Advances in the Astronautical Sciences. Vol. 149 Univelt Inc., 2013. p. 403-416.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Larson, K, Gaylor, D & Winkler, S 2013, Worst-case GPS constellation for testing navigation at geosynchronous orbit for GOES-R. in Advances in the Astronautical Sciences. vol. 149, Univelt Inc., pp. 403-416, 2013 36th Annual AAS Rocky Mountain Section Guidance and Control Conference, Guidance and Control 2013, Breckenridge, CO, United States, 2/1/13.
Larson K, Gaylor D, Winkler S. Worst-case GPS constellation for testing navigation at geosynchronous orbit for GOES-R. In Advances in the Astronautical Sciences. Vol. 149. Univelt Inc. 2013. p. 403-416
Larson, Kristin ; Gaylor, David ; Winkler, Stephen. / Worst-case GPS constellation for testing navigation at geosynchronous orbit for GOES-R. Advances in the Astronautical Sciences. Vol. 149 Univelt Inc., 2013. pp. 403-416
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