The monitoring device includes a unit for determining the current position (Pc) of the space- or aircraft (10), during a flight of the space- or aircraft (10) along a predetermined reference trajectory (TR), a unit for calculating a first distance (DO) between said current position (Pc) and a theoretical position (PO) corresponding to the position of the space- or aircraft (10) on said predetermined reference trajectory (TR), a unit for calculating a second distance (D1) on the basis of a predetermined uncertainty of the position determining unit, a unit for summing the first distance (DO) and the second distance (D1) so as to calculate a comparison value (RP), a unit for comparing the comparison value (RP) with a predetermined limit (L1), the predetermined limit (L1) being associated with the predetermined reference trajectory (TR), and a unit for transmitting an alert message if said comparison value (RP) is higher than said limit (L1).


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    Title :

    PROCÉDÉ ET DISPOSITIF DE SURVEILLANCE DE L'INTÉGRITÉ D'UNE TRAJECTOIRE D'UN ENGIN VOLANT, SPATIAL OU AÉRIEN


    Additional title:

    METHOD AND DEVICE FOR MONITORING THE INTEGRITY OF A TRAJECTORY OF A SPACE- OR AIRCRAFT
    VERFAHREN UND VORRICHTUNG ZUR ÜBERWACHUNG DER INTEGRITÄT DER FLUGBAHN EINES RAUM- ODER LUFTFAHRZEUGS


    Contributors:

    Publication date :

    2020-01-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS




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