Provided are a flight simulation and control method of a unmanned aerial vehicle with regenerative fuel cells and solar cells for high altitude long endurance, and a control apparatus thereof. The high altitude long endurance simulation method for an unmanned aerial vehicle based on regenerative fuel cells and solar cells includes: a variable inputting step of inputting design variables of the unmanned aerial vehicle based on regenerative fuel cells and solar cells; a modeling step of performing modeling of the unmanned aerial vehicle based on regenerative fuel cells and solar cells using the design variables input in the variable inputting step; and an analyzing step of analyzing a modeling result in the modeling step to perform a high altitude long endurance simulation while controlling any one of the design variables input in the variable inputting step.


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    Title :

    FLIGHT SIMULATION AND CONTROL METHOD OF A UNMANNED AERIAL VEHICLE WITH REGENERATIVE FUEL CELLS AND SOLAR CELLS FOR HIGH ALTITUDE LONG ENDURANCE, AND A CONTROL APPARATUS THEREOF


    Contributors:
    KIM MINJIN (author) / SOHN YOUNG-JUN (author) / KIM SEUNG-GON (author) / PARK GU-GON (author) / BAE BYUNGCHAN (author) / YIM SUNG-DAE (author) / PARK SEOK-HEE (author) / YANG TAE-HYUN (author) / LEE WON-YONG (author) / KIM CHANG-SOO (author)

    Publication date :

    2017-11-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen