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Post-Flight Assessment of Low Density Supersonic Decelerator Flight Dynamics Test 2 SimulationNASA's Low Density Supersonic Decelerator (LDSD) project conducted its second Supersonic Flight Dynamics Test (SFDT-2) on June 8, 2015. The Program to Optimize Simulated Trajectories II (POST2) was one of the flight dynamics tools used to simulate and predict the flight performance and was a major tool used in the post-flight assessment of the flight trajectory. This paper compares the simulation predictions with the reconstructed trajectory. Additionally, off-nominal conditions seen during flight are modeled in the simulation to reconcile the predictions with flight data. These analyses are beneficial to characterize the results of the flight test and to improve the simulation and targeting of the subsequent LDSD flights.
Document ID
20160007702
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Dutta, Soumyo
(NASA Langley Research Center Hampton, VA, United States)
Bowes, Angela L.
(NASA Langley Research Center Hampton, VA, United States)
White, Joseph P.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Striepe, Scott A.
(NASA Langley Research Center Hampton, VA, United States)
Queen, Eric M.
(NASA Langley Research Center Hampton, VA, United States)
O'Farrel, Clara
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Ivanov, Mark C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
June 20, 2016
Publication Date
February 14, 2016
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NF1676L-22643
AAS Paper 16-222
Report Number: NF1676L-22643
Report Number: AAS Paper 16-222
Meeting Information
Meeting: AAS/AIAA Space Flight Mechanics Meeting
Location: Napa, CA
Country: United States
Start Date: February 14, 2016
End Date: February 18, 2016
Sponsors: American Inst. of Aeronautics and Astronautics, American Astronomical Society, American Astronautical Society
Funding Number(s)
WBS: WBS 406979.01.07.06
Distribution Limits
Public
Copyright
Public Use Permitted.
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