The functional mockup test of the flight control system of ASKA with the stability and control augmentation systems is described. The tests made included software verification, simulated failure effects testing, closed loop test, and piloted simulation test. The results show that the functions and performance of the control system are satisfactory for flight safety of ASKA.


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    Title :

    Functional Mock-Up Test of the Flight Control System of the NAL (National Aerospace Laboratory) QSTOL Research Aircraft ASKA


    Contributors:
    T. Uchida (author) / A. Tada (author) / N. Okada (author) / H. Yamato (author) / T. Ogawa (author)

    Publication date :

    1988


    Size :

    64 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English