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 current value of a control parameter which is representative of the roll control surfaces of the aircraft, and of a current a...

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Bibliographische Detailangaben
Hauptverfasser:	CHATRENET, DOMINIQUE, BOE, REGIS
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIRCRAFT 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 PARACHUTES PERFORMING OPERATIONS PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS 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 current 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. Procédé et dispositif de détection d'une dissymétrie latérale d'un aéronef . Le dispositif de détection (1) comporte un moyen (7) pour détecter une dissymétrie latérale, en fonction de la valeur courante d'un paramètre de commande qui est représentatif des surfaces de commande de roulis de l'aéronef, et d'un angle de déflexion courant d'un manche latéral de l'aéronef .