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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 (AIAA 2014-2534)



    Kongress:

    19th, AIAA international space planes and hypersonic systems and technologies conference ; 2014 ; Atlanta, GA



    Erscheinungsdatum :

    01.01.2014


    Format / Umfang :

    15 pages


    Anmerkungen:

    Includes bibliographical references and author index



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





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