Aircraft tailstrike avoidance system

The invention relates to a method for reducing the likelihood of an aircraft tail strike in an aircraft flight control system (16) having a normal pitch command signal provided to a pitch control device (18) for altering the aircraft's pitch attitude, the method comprising: (a) determining a cu...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	EVANS, MONTE R, WELLS, STEPHEN L, DEWITT, WENDI M
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	CONTROLLING PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
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