Method and device for detecting a lateral dissymmetry of an aircraft

Method and device for detecting a lateral dissymmetry of an aircraft. The detection device (1) comprises a means (7) for detecting a lateral dissymmetry, as a function of the cement value of a control parameter which is representative of the roll control surfaces of the aircraft, and of a current an...

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Bibliographische Detailangaben
Hauptverfasser:	BOE REGIS, CHATRENET DOMINIQUE
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIRCRAFT ALARM SYSTEMS ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GYROSCOPIC INSTRUMENTS MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION ORDER TELEGRAPHS PARACHUTES PERFORMING OPERATIONS PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS SIGNALLING SIGNALLING OR CALLING SYSTEMS SURVEYING TESTING TRANSPORTING
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Beschreibung
Zusammenfassung:	Method and device for detecting a lateral dissymmetry of an aircraft. The detection device (1) comprises a means (7) for detecting a lateral dissymmetry, as a function of the cement value of a control parameter which is representative of the roll control surfaces of the aircraft, and of a current angle of deflection of a lateral stick of the aircraft.