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InSight Entry, Descent and Landing Post-Flight Performance AssessmentOn November 26, 2018, the Interior Exploration using Seismic Investigations, Geodesy and Heat Transport (InSight) lander successfully touched down on the surface of Mars. NASA Langley Research Center’s (LaRC) Program to Optimize Simulated Trajectories II (POST2) was used during both project development and flight operations to assess the Entry, Descent and Landing (EDL) vehicle performance against related requirements across the expected range of possible environmental and spacecraft conditions. During flight operations, these analyses were used to evaluate the need for updating flight software EDL parameters and the effects of executing a trajectory correction maneuver (TCM). Therefore, the NASA LaRC POST2 simulation had a critical role during the cruise, approach and ultimately EDL phases of the mission. This paper presents results of the final pre- and post- EDL flight performance assessments. A summary of the reconstructed “as-flown” trajectory with a comparison of key EDL metrics to the nominal and three-sigma bound pre-EDL predictions is also provided. Emphasis on the trajectory between entry interface and parachute deploy is provided as this is the period during which deviations from the pre-EDL prediction occurred. The post-flight assessment provides important verification of the POST2 models and analysis techniques used for InSight, providing critical feed-forward information to future lander missions.
Document ID
20200002909
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Robert W Maddock
(Langley Research Center Hampton, Virginia, United States)
Alicia M Dwyer Cianciolo
(Langley Research Center Hampton, Virginia, United States)
Ashley M Korzun
(Langley Research Center Hampton, Virginia, United States)
Daniel K Litton
(Langley Research Center Hampton, Virginia, United States)
Carlie H Zumwalt
(Langley Research Center Hampton, Virginia, United States)
Chris D Karlgaard ORCID
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Date Acquired
April 22, 2020
Publication Date
January 6, 2020
Publication Information
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NF1676L-33361
AIAA 2020-1270
Report Number: NF1676L-33361
Meeting Information
Meeting: AIAA SciTech Exhibition and Forum
Location: Orlando, FL
Country: US
Start Date: January 6, 2020
End Date: January 10, 2020
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 336763.01.04.15
Distribution Limits
Public
Copyright
Public Use Permitted.
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