Time optimal trajectoris for the P-3C ASW aircraft are developed. The optimization program is based on the use of the Energy State Approximation and a unique graphical construct. Certain features of the program are verified by comparison to NATOPS manual flight test results, while verification of the actual time savings reported requires implementation of a recommended flight test program. This study establishes that flight path optimization procedures and a minimal data base can now be used in improving operational performance. For the P-3C application, increases in the average transit speeds of up to to 70 knots were demonstrated.


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    Title :

    VP Optimum Flight Path


    Contributors:

    Publication date :

    1971


    Size :

    105 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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