The paper examines, from the problem formulation aspect, a fundamental scheme for semiautomatic control of the airplane in the transition regimes, which provides both reliable control of the airplane by the pilot and automatic stabilization of the airplane relative to the center of gravity.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    VTOL Airplane Control in Transition Regimes


    Contributors:

    Publication date :

    1974


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    X-14 VTOL airplane -- Design tool

    O'Malley, Jr., J.A. | Engineering Index Backfile | 1958


    X-14 VTOL airplane -- Design tool

    Williams, C. | Engineering Index Backfile | 1957


    Design aspects of bell aircraft VTOL airplane

    O'Malley, Jr., J.A. | Engineering Index Backfile | 1955


    A VTOL-CAPABLE AIRPLANE HAVING ANGLED PROPULSORS

    POH CHUNG-KIAK / POH CHUNG-HOW | European Patent Office | 2020

    Free access

    Design aspects of bell aircraft VTOL airplane

    O'Malley, Jr., J.A. | Engineering Index Backfile | 1955