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Post-Flight EDL Entry Guidance for the Mars 2020 MissionLike its predecessor Mars Science Laboratory, the Mars 2020 mission successfully utilized a derivative of the Apollo Entry Terminal Point Controller guidance algorithm, whereby bank angle controls range flown along a trajectory. The flight performance of this algorithm in conjunction with a range-trigger for parachute deploy delivered the Perseverance rover to 1.7 km from the expected touchdown location within an ellipse of 7.5 x 5.2 km. This miss distance is largely attributed to atmospheric and aerodynamic modeling uncertainties between the design and as-flown trajectory. This algorithm for guided entry continues to provide a solid basis for Mars missions to improve upon.
Document ID
20250000207
Acquisition Source
Johnson Space Center
Document Type
Presentation
Authors
Lynn McGrew
(Johnson Space Center Houston, United States)
Brian Killeen
(Johnson Space Center Houston, United States)
Gavin Mendeck
(Johnson Space Center Houston, United States)
Date Acquired
January 7, 2025
Subject Category
Computer Programming and Software
Spacecraft Design, Testing and Performance
Meeting Information
Meeting: 35th AAS/AIAA Space Flight Mechanics Meeting
Location: Kaua'i, HI
Country: US
Start Date: January 19, 2025
End Date: January 23, 2025
Sponsors: American Institute of Aeronautics and Astronautics, American Astronautical Society
Funding Number(s)
WBS: 829688.13.06.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
Guidance
Mars2020
Post-Flight Performance
GNC
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