DocumentCode
2208159
Title
Operational use of GPS navigation for space shuttle entry
Author
Goodman, John L. ; Propst, Carolyn A.
Author_Institution
United Space Alliance, LLC, Houston, TX
fYear
2008
fDate
5-8 May 2008
Firstpage
731
Lastpage
743
Abstract
The STS-118 flight of the Space Shuttle Endeavour was the first shuttle mission flown with three Global Positioning System (GPS) receivers in place of the three legacy Tactical Air Navigation (TACAN) units. This marked the conclusion of a 15 year effort involving procurement, missionization, integration, and flight testing of a GPS receiver and a parallel effort to formulate and implement shuttle computer software changes to support GPS. The use of GPS data from a single receiver in parallel with TACAN during entry was successfully demonstrated by the orbiters Discovery and Atlantis during four shuttle missions in 2006 and 2007. This provided the confidence needed before flying the first all GPS, no TACAN flight with Endeavour. A significant number of lessons were learned concerning the integration of a software intensive navigation unit into a legacy avionics system. These lessons have been taken into consideration during vehicle design by other flight programs, including the vehicle that will replace the Space Shuttle, Orion.
Keywords
Global Positioning System; avionics; radio receivers; space vehicles; Atlantis; Discovery; GPS navigation; Global Positioning System receivers; Orion; STS-118 flight; Space Shuttle Endeavour; Tactical Air Navigation units; avionics system; shuttle computer software; space shuttle entry; Aerospace electronics; Certification; Delay; Global Positioning System; Humans; Navigation; Procurement; Space shuttles; Space vehicles; Switches;
fLanguage
English
Publisher
ieee
Conference_Titel
Position, Location and Navigation Symposium, 2008 IEEE/ION
Conference_Location
Monterey, CA
Print_ISBN
978-1-4244-1536-6
Electronic_ISBN
978-1-4244-1537-3
Type
conf
DOI
10.1109/PLANS.2008.4570031
Filename
4570031
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