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The Best Estimated Trajectory Analysis for Pad Abort OneI. Best Estimated Trajectory (BET) objective: a) Produce reconstructed trajectory of the PA-1 flight to understand vehicle dynamics and aid other post flight analyses. b) Leverage all measurement sources taken of vehicle during flight to produce the most accurate estimate of vehicle trajectory. c) Generate trajectory reconstructions of the Crew Module (CM), Launch Abort System (LAS), and Forward Bay Cover (FBC). II. BET analysis was started immediately following the PA-1 mission and was completed in September, 2010 a) Quick look version of BET released 5/25/2010: initial repackaging of SIGI data. b) Preliminary version of BET released 7/6/2010: first blended solution using available sources of external measurements. c) Final version of BET released 9/1/2010: final blended solution using all available sources of data.
Document ID
20110010892
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Kutty, Prasad
(Analytical Mechanics Associates, Inc. Edwards, CA, United States)
Noonan, Meghan
(Analytical Mechanics Associates, Inc. Edwards, CA, United States)
Karlgaard, Christopher
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Beck, Roger
(Analytical Mechanics Associates, Inc. Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
January 4, 2011
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
DFRC-E-DAA-TN2681
Report Number: DFRC-E-DAA-TN2681
Meeting Information
Meeting: 49th AIAA Aerospace Sciences Meeting
Location: Orlando, FL
Country: United States
Start Date: January 4, 2011
End Date: January 7, 2011
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 644423.10.36.01.05
CONTRACT_GRANT: NND07AA24Z
Distribution Limits
Public
Copyright
Public Use Permitted.
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