NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Entry Trajectory and Atmosphere Reconstruction Methodologies for the Mars Exploration Rover MissionThe Mars Exploration Rover (MER) mission will land two landers on the surface of Mars, arriving in January 2004. Both landers will deliver the rovers to the surface by decelerating with the aid of an aeroshell, a supersonic parachute, retro-rockets, and air bags for safely landing on the surface. The reconstruction of the MER descent trajectory and atmosphere profile will be performed for all the phases from hypersonic flight through landing. A description of multiple methodologies for the flight reconstruction is presented from simple parameter identification methods through a statistical Kalman filter approach.
Document ID
20040031558
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Desai, Prasun N.
(NASA Langley Research Center Hampton, VA, United States)
Blanchard, Robert C.
(George Washington Univ. Hampton, VA, United States)
Powell, Richard W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2003
Subject Category
Lunar And Planetary Science And Exploration
Meeting Information
Meeting: International Workshop on Planetary Probe Atmospheric Entry and Descent Trajectory Analysis and Science
Location: Lisbon
Country: Portugal
Start Date: October 6, 2003
End Date: October 9, 2003
Funding Number(s)
OTHER: 149-30-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available