A method and apparatus for controlling a flight of an aircraft. An undesired change in an airspeed for the aircraft is identified. A number of commands for a flight control system associated with a wing of the aircraft are identified in response to the undesired change in the airspeed. The number of commands is configured to cause the flight control system to maintain a lift of the aircraft for a desired trajectory.


    Access

    Download


    Export, share and cite



    Title :

    Flight trajectory compensation system for airspeed variations


    Contributors:

    Publication date :

    2017-11-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen




    Conversion between calibrated airspeed and true airspeed in trajectory modeling

    PROSSER KEVIN | European Patent Office | 2021

    Free access

    CONVERSION BETWEEN CALIBRATED AIRSPEED AND TRUE AIRSPEED IN TRAJECTORY MODELING

    PROSSER KEVIN | European Patent Office | 2019

    Free access

    Flight Evaluation: Rosemount Orthogonal Low Airspeed System Low Airspeed Sensor

    R. P. Jefferis / J. C. O'Connor / J. R. Bullock | NTIS | 1974


    CONVERSION BETWEEN CALIBRATED AIRSPEED AND TRUE AIRSPEED IN TRAJECTORY MODELING

    PROSSER KEVIN | European Patent Office | 2024

    Free access