An aircraft control system is described which is particularly suited to rotary wing aircraft. Longitudinal acceleration and course rate commands are derived from a manual control stick to control translational velocity of the aircraft along a flight path. In the collective channel the manual controls provide vertical velocity commands. In the yaw channel the manual controls provide sideslip or heading rate commands at high or low airspeeds, respectively. The control system permits pilots to fly along prescribed flight paths in a precise manner with relatively low work load.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aircraft Control System


    Contributors:

    Publication date :

    1973


    Size :

    8 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Aircraft onboard control system, aircraft control system and aircraft

    HU HUAZHI / XUE PENG | European Patent Office | 2022

    Free access

    AIRCRAFT CONTROL SYSTEM, AIRCRAFT CONTROL METHOD, AND AIRCRAFT

    MIYAWAKI TAKASHI / ABE MASAKATSU / KATO HIROKI | European Patent Office | 2019

    Free access

    AIRCRAFT CONTROL SYSTEM, AIRCRAFT CONTROL METHOD AND AIRCRAFT

    MIYAWAKI TAKASHI / ABE MASAKATSU / KATO HIROMOTO | European Patent Office | 2019

    Free access

    Aircraft control system, aircraft control method, and aircraft

    MIYAWAKI TAKASHI / ABE MASAKATSU / KATO HIROKI | European Patent Office | 2022

    Free access

    AIRCRAFT CONTROL DEVICE, AIRCRAFT CONTROL SYSTEM, AND AIRCRAFT CONTROL METHOD

    NISHIYAMA JOJI / KOAMI YASUAKI / ARAI KANEHIDE | European Patent Office | 2019

    Free access