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    Titel :

    Effect of Initial Flight Path Angle Error and Control Constraint on the Optimized Ascent Trajectory of a Typical Launch Vehicle


    Beteiligte:
    Joshi, Ashok (Autor:in) / Sudhir Kumar, B. (Autor:in)

    Kongress:

    19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference



    Erscheinungsdatum :

    2014-01-01



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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