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    Title :

    Effect of Initial Flight Path Angle Error and Control Constraint on the Optimized Ascent Trajectory of a Typical Launch Vehicle (AIAA 2014-2534)



    Conference:

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



    Publication date :

    2014-01-01


    Size :

    15 pages


    Remarks:

    Includes bibliographical references and author index



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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