CLOSED LOOP LOAD FORCE ESTIMATION SYSTEMS AND METHODS

What is described is a system for determining a force applied to an outer disc (110) of an aircraft brake by an actuator motor (206). The system includes a current sensor (208) coupled to the actuator motor and configured to detect a detected amount of current applied to the actuator motor. The syst...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	KOLK, Richard, SINGH, Sameep
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL BLASTING BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL BRAKES CLUTCHES COUPLINGS FOR TRANSMITTING ROTATION ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OFVEHICLES THERMAL INSULATION IN GENERAL TRANSPORTING VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES VEHICLES IN GENERAL WEAPONS
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Beschreibung
Zusammenfassung:	What is described is a system for determining a force applied to an outer disc (110) of an aircraft brake by an actuator motor (206). The system includes a current sensor (208) coupled to the actuator motor and configured to detect a detected amount of current applied to the actuator motor. The system also includes a controller coupled to the current sensor (208). The controller is configured to determine an estimated current. The controller is also configured to receive the detected amount of current. The controller is also configured to determine an adjusted current based on the detected amount of current and the estimated current. The controller is also configured to determine an estimate of the force applied to the outer disc (110) based on the adjusted current.