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Mars Smart Lander Simulations for Entry, Descent, and LandingTwo primary simulations have been developed and are being updated for the Mars Smart Lander Entry, Descent, and Landing (EDL). The high fidelity engineering end-to-end EDL simulation that is based on NASA Langley's Program to Optimize Simulated Trajectories (POST) and the end-to-end real-time, hardware-in-the-loop simulation testbed, which is based on NASA JPL's (Jet Propulsion Laboratory) Dynamics Simulator for Entry, Descent and Surface landing (DSENDS). This paper presents the status of these Mars Smart Lander EDL end-to-end simulations at this time. Various models, capabilities, as well as validation and verification for these simulations are discussed.
Document ID
20030000914
Acquisition Source
Headquarters
Document Type
Preprint (Draft being sent to journal)
Authors
Striepe, S. A.
(NASA Langley Research Center Hampton, VA United States)
Way, D. W.
(NASA Langley Research Center Hampton, VA United States)
Balaram, J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
AIAA Paper 2002-4412
Report Number: AIAA Paper 2002-4412
Meeting Information
Meeting: AIAA Atmospheric Flight Mechanics Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: August 5, 2002
End Date: August 8, 2002
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available