The invention relates to an automatic carrier landing composite control method of carrier airflow compensation-containing carrier-borne aircraft, and belongs to the technical field of flight control. The automatic carrier landing composite control method is implemented mainly through composite control of four modules, including an elevator channel control law module, an accelerator channel control law module, an aileron channel control law module and a rudder channel control law module. In the automatic carrier landing composite control method, feedforward control is performed by using glide path future information, feedback control is performed by using carrier-borne aircraft current information, and average operation can be performed on a control plane and an accelerator of a carrier-borne aircraft in advance so as to achieve a tracking compensating purpose, reduce instantaneous energy, increase the response speed and ensure safe carrier landing of the carrier-borne aircraft on an aircraft carrier.


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    Title :

    Automatic carrier landing composite control method of carrier airflow compensation-containing carrier-borne aircraft


    Contributors:
    ZHEN ZIYANG (author) / SHAO MINMIN (author) / GONG HUAJUN (author) / WANG XINHUA (author) / JIANG JU (author)

    Publication date :

    2015-07-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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