A pilot controlled stability control system is described that employs direct lift control (spoiler control) with elevator control to control the flight path angle of an aircraft. A computer on the aircraft generates an elevator control signal and a spoiler control signal, using a pilot-controlled pitch control signal and pitch rate, vertical velocity, roll angle, groundspeed, engine pressure ratio and vertical acceleration signals which are generated on the aircraft. The direct lift control by the aircraft spoilers improves the response of the aircraft flight path angle and provides short term flight path stabilization against environmental disturbances.


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    Title :

    A Velocity Vector Control System Augmented with Direct Lift Control


    Contributors:

    Publication date :

    1979


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Velocity vector control system augmented with direct lift control

    Tisdale, H. F., Sr. / Kelly, W. W. | NTRS | 1981



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