Oscillatory failure detecting method for aircraft i.e. transport aircraft, involves estimating value of parameter of behaviour model of control surface by realizing joint estimation of state illustrated by theoretical position and parameter
FR2919268A1
SHIPPING PLANE
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Perfected current sensor
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Trapper equipped with at least one locking spacer capable of being actioned on each side of the trap.
FR2918349A1
System for displaying avionic and non-avionic applications
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Computer maintenance system of an aircraft
FR2917201A1
Method and device for managing, processing and controlling parameters used on aircraft
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Apparatus for handling an aircraft turbopropulser comprising hydraulic fastening means.
FR2916546A1
Method for simulating an on-board aircraft on-board system for testing an operating software and device for implementing said method
FR2916424A1
Aircraft engine attaching machine comprising a biaise shim for attaching the front engine attachment
FR2916548A1
Device for assistance in decision making concerning the capacity of an aircraft to start a flight.
FR2916530A1
Method and device for monitoring position indication of an aircraft
FR2916547A1
Method and device for detecting oscillatory failures relating to an aircraft government serving chain.
FR2916060A1
Method and device for monitoring a horizontal position of an aircraft on the ground
FR2915178A1
Attachment of a mat box on a sail, pincing a side panel of the housing
FR2915238A1
Method and system for starting a cold weather turbomoteur.
FR2915179A1
Aircraft with reduced environmental impact.
FR2915176A1
Engine attaching machine for an aircraft having a rear engine attachment having a barrel nut
FR2915175A1
Engine attaching machine for an aircraft having a rear engine attachment beam deportee from the housing
FR2915177A1
Aircraft engine and aircraft engine clamping device comprising at least one such device
