A method for adjusting the angular position of a wheel, in particular a wheel of a landing gear on an aircraft. The wheel being connected to at least one hydraulic cylinder controlled by a servo valve. The method comprising a step for determining an angular deviation between a measurement of the angular position and a setpoint angular position, a first proportional correction step, a second integral correction step and a step for adding the first current and the second current in order to determine a control current of the servo valve. The second integral control step comprising a sub-step for limiting the second current according to a parametric law imposing a second current of zero value when the angular deviation is less, in absolute value, than a first determined threshold.
METHOD FOR ADJUSTING THE ANGULAR POSITION OF A WHEEL, IN PARTICULAR A WHEEL OF AN AIRCRAFT LANDING GEAR
01.02.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Method for adjusting angular position of wheel, in particular of aircraft landing gear
Europäisches Patentamt | 2023
|Europäisches Patentamt | 2025
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