METHOD AND SYSTEM FOR DETERMINING THE LONGITUDINAL POSITION OF THE CENTER OF GRAVITY OF AN AIRCRAFT PROVIDED WITH ADJUSTABLE HORIZONTAL TENSION AND APPLICATION TO THE SURVEILLANCE OF SAID CENTER OF GRAVITY IN THE NEIGHBORHOOD OF THE AIRCRAFT FOCUS

摘要

P THE INVENTION IS REMARKABLE IN THAT, AT A FLIGHT POINT FOR WHICH THIS AIRCRAFT 1 IS IN BALANCE WITH ITS DEPTH OF GAUVE 5 IN AERODYNAMIC EXTENSION OF THE ADJUSTABLE HORIZONTAL ADJUSTMENT 4 AND WHEN THIS CENTER OF GRAVITY IS IN THE NEIGHBORHOOD OF THE FIREPLACE DUDIT AERONEF, CALCULATES THE POSITION OF THE CENTER OF GRAVITY FROM: - POSITION X OF THE FOCUS F DUDIT AIRCRAFT 1; - MEASUREMENT OF THE IH STROKE OF THE ADJUSTABLE HORIZONTAL ADJUSTMENT 4; - A FIRST FUNCTION K, M, N1 OF THE REGIME N1 OF THE ENGINES 3 OF THE AIRCRAFT AND THE NUMBER OF MACH M; AND - A SECOND FUNCTION OF SAID NUMBER OF MACH. / P P APPLICATION TO MONITORING THE CENTER OF GRAVITY OF AN AIRCRAFT IN FLIGHT / P