Mars Smart Lander Simulations for Entry, Descent, and Landing
Author(s) -
Scott A. Striepe,
Bob Balaram,
David W. Way,
Alicia Dwyer
Publication year - 2002
Publication title -
aiaa atmospheric flight mechanics conference and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2002-4412
Subject(s) - mars exploration program , descent (aeronautics) , astrobiology , mars landing , moon landing , aerospace engineering , exploration of mars , computer science , geology , aeronautics , environmental science , engineering , physics , apollo , zoology , biology
Two 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.
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