□ TPA frame work for obtaining trajectory performance bound of individual aircraft is proposed □ Fixed RTA suboptimal trajectory generation method is proposed □ Trajectory structure is designed by analysis of real optimal trajectory □ The suboptimal trajectory shows the similar performance comparing to real optimal trajectory


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    Title :

    Fixed RTA fuel optimal profile descent based on analysis of trajectory performance bound


    Contributors:


    Publication date :

    2012-10-01


    Size :

    1987638 byte





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English