CALCULATION AND DISPLAY OF WARNING SPEED FOR THRUST ASYMMETRY CONTROL

A system and a method for calculating and then displaying a minimum safe flight speed for an aircraft to maintain control under conditions of thrust asymmetry, and for providing flight path guidance and autopilot commands to maintain airspeed above this calculated minimum speed. The software of a fl...

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Hauptverfasser: EGGOLD, DAVID P, BRESLEY, WILLIAM M, FLANNIGAN, SEAN J, WIEDEMANN, JOHN, GARDNER, KYLE, MALLOUK, BECHARA J, CHEN, SHERWIN S, HARRIGAN, JEFFERY S
Format: Patent
Sprache:eng ; fre
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