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Orion Exploration Flight Test 1 (EFT-1) Best Estimated Trajectory DevelopmentThe Orion Exploration Flight Test 1 (EFT-1) mission successfully flew on Dec 5, 2014 atop a Delta IV Heavy launch vehicle. The goal of Orions maiden flight was to stress the system by placing an uncrewed vehicle on a high-energy trajectory replicating conditions similar to those that would be experienced when returning from an asteroid or a lunar mission. The Orion navigation team combined all trajectory data from the mission into a Best Estimated Trajectory (BET) product. There were significant challenges in data reconstruction and many lessons were learned for future missions. The team used an estimation filter incorporating radar tracking, onboard sensors (Global Positioning System and Inertial Measurement Unit), and day-of-flight weather balloons to evaluate the true trajectory flown by Orion. Data was published for the entire Orion EFT-1 flight, plus objects jettisoned during entry such as the Forward Bay Cover. The BET customers include approximately 20 disciplines within Orion who will use the information for evaluating vehicle performance and influencing future design decisions.
Document ID
20160001184
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Holt, Greg N.
(NASA Johnson Space Center Houston, TX, United States)
Brown, Aaron
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
January 26, 2016
Publication Date
February 5, 2016
Subject Category
Astrodynamics
Spacecraft Instrumentation And Astrionics
Report/Patent Number
AAS 16-117
JSC-CN-35079
Meeting Information
Meeting: Annual AAS Guidance and Control Conference
Location: Breckenridge, CO
Country: United States
Start Date: February 5, 2016
End Date: February 10, 2016
Sponsors: American Astronautical Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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