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Spaceborne Global Positioning System for SpacecraftThe spaceborne Global Positioning System receiver provides navigational solutions and is designed for use in low Earth orbit. The spaceborne GPS receiver can determine the orbital position of a spacecraft using any of the satellites wi thin the GPS constellation. It is a multiple processor system incorporating redundancy by using a microcontroller to handle the closure of tracking loops for acquired GPS satellites, while a separate microprocessor computes the spacecraft navigational solution and handles other tasks within the receiver. 'Me spaceborne GPS receiver can use either microcontroller or the microprocessor to close the satellite tracking loops. The use of microcontroller provides better tracking performance of acquired GPS satellites. The spaceborne GPS receiver utilizes up to seven separate GPS boards, with each board including its own set of correlators, down-converters and front-end components. The spaceborne GPS receiver also includes telemetry and time-marking circuitry. The spaceborne GPS receiver communicates with other spacecraft systems through a variety of interfaces and can be software-configured to support several different mission profiles.
Document ID
20010117890
Acquisition Source
Goddard Space Flight Center
Document Type
Other - Patent
Authors
Lamar F Dougherty
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Frederick A Niles
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Miriam D Wennersten
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Havre DeGrace
(Goddard Space Flight Center Greenbelt, Maryland, United States)
Date Acquired
August 20, 2013
Publication Date
April 3, 2001
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-Case-GSC-13991-1|US-Patent-6,211,822
Patent Application
US-Patent-Appl-SN-348876|US-Patent-Appl-SN-092491
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