AIRCRAFT MONITORING SYSTEM

PROBLEM TO BE SOLVED: To provide a method and apparatus for monitoring operation of a control surface of an aircraft during a flight test.SOLUTION: A pilot control input signal 204 is received. A response of a control surface system 206 controlled by a flight control model 230 is identified using th...

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Bibliographische Detailangaben
Hauptverfasser:	DARREN GORDON MCDONALD, SEAN M PENNELL, NOAH ERIC AARON
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a method and apparatus for monitoring operation of a control surface of an aircraft during a flight test.SOLUTION: A pilot control input signal 204 is received. A response of a control surface system 206 controlled by a flight control model 230 is identified using the pilot control input signal 224. An alert 240 is generated when the control surface system 206 reaches a threshold 241 with respect to the control surface system 206 becoming saturated.