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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Mars Smart Lander Simulations for Entry, Descent, and Landing


    Contributors:
    Striepe, S. A. (author) / Way, D. W. (author) / Balaram, J. (author)

    Conference:

    AIAA Atmospheric Flight Mechanics Conference and Exhibit ; 2002 ; Monterey, CA, United States


    Publication date :

    2002-01-01


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English




    Mars Smart Lander Simulations for Entry, Descent, and Landing

    Striepe, Scott / Balaram, Bob / Way, David et al. | AIAA | 2002


    Mars Smart Lander Simulations for Entry, Descent, and Landing

    S. A. Striepe / D. W. Way / J. Balaram | NTIS | 2002


    MARS smart lander simulations for entry, descent, and landing

    Dwyer, A. M. / Way, D. W. / Stiepe, S. A. et al. | NTRS | 2002


    AIAA-2002-4412 Mars Smart Lander Simulations for Entry, Descent, and Landing

    Striepe, S. / Balaram, B. / Way, D. et al. | British Library Conference Proceedings | 2002