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Reconstruction of the Adaptable Deployable Entry and Placement Technology Sounding Rocket One Flight TestThe Adaptable Deployable Entry and Placement Technology Sounding Rocket One flight test is a demonstration experiment for deployable atmospheric decelerator technologies. The suborbital flight test occurred on 12 September 2018, at the White Sands Missile Range. Data from on-board and ground-based sensors were collected, from which the as-flown trajectory was reconstructed using an iterative extended Kalman filter-smoother. This paper describes the methodology, test vehicle instrumentation, and data analysis results from the flight test trajectory reconstruction.


Document ID
20200002413
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Tynis, Jake A.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Karlgaard, Christopher D.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Williams, Joseph D.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Dutta, Soumyo
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
April 14, 2020
Publication Date
January 7, 2019
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NF1676L-30323
Report Number: NF1676L-30323
Funding Number(s)
WBS: 394364.04.20.23
Distribution Limits
Public
Copyright
Public Use Permitted.
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