An airborne platform includes an avionics controller circuit. The avionics controller circuit is configured to receive an ownship orientation from a sensor configured to detect the ownship orientation. The avionics controller circuit is configured to determine an orientation parameter based on the ownship orientation. The avionics controller circuit is configured to compare the orientation parameter to an orientation threshold. The avionics controller circuit is configured to determine the ownship to be in a wake vortex condition based on at least one wake vortex criteria, the at least one wake vortex criteria including the orientation parameter being greater than the orientation threshold for more than a predetermined period of time.


    Access

    Download


    Export, share and cite



    Title :

    System and method for recovery from wake vortex encounters


    Contributors:

    Publication date :

    2020-10-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Accidents Resulting from Wake Vortex Encounters

    Passman, R. H. / Flight Safety Foundation | British Library Conference Proceedings | 1995


    Modeling of Wake-vortex Aircraft Encounters

    Smith, Sonya T. | NTRS | 1999



    Hazard criteria for wake vortex encounters

    Sammonds, R. I. / Stinnett, G. W., Jr. | NTRS | 1975


    Hazard criteria for wake vortex encounters

    Sammonds, R. I. / Stinnett, G. W., Jr. / Larsen, W. E. | NTRS | 1976