This presentation details work performed during the Fall 2011 term in the Research Controls and Dynamics Branch at NASA Dryden Flight Research Center. Included is a study on a possible landing footprint algorithm, with direct application to the HTV-2. Also discussed is work in support of the MIPCC effort, which includes optimal trajectory solutions for the F-15A Streak Eagle aircraft and theoretical performance of an F-15A with a MIPCC propulsion system.


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    Title :

    Implementation of a Landing Footprint Algorithm for the HTV-2 and Trajectory Simulations


    Contributors:

    Publication date :

    2012-04-30


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :