SYSTEME D'ACTIONNEMENT D'UNE SURFACE DE CONTROLE D'UN AERONEF, ET PROCEDE ASSOCIE

The system has first and second electromechanical actuators (2, 3) to generate first and second forces to move an aileron. First and second force sensors (14, 15) respectively generate first and second force measurement signals proportional to the forces. An electronic control unit (4) generates a f...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	PUJOS MATTHIEU
Format:	Patent
Sprache:	fre
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING COSMONAUTICS FUNCTIONAL ELEMENTS OF SUCH SYSTEMS HELICOPTERS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	The system has first and second electromechanical actuators (2, 3) to generate first and second forces to move an aileron. First and second force sensors (14, 15) respectively generate first and second force measurement signals proportional to the forces. An electronic control unit (4) generates a first actuator control signal based on a first actuator position measurement signal proportional to a measured position of the first actuator, and a measured position correction signal based on a difference between the force measurement signals to eliminate permanent variation between the forces. An independent claim is also included for a method for actuating a control surface of an aircraft.