Control method for an electrical braking system and electrical braking system for aircraft
A control method of an electrical braking system for aircraft includes a plurality of electromechanical actuators capable of applying a braking force on friction members. Each electromechanical actuator includes an electric motor equipped with one or more windings. The braking system further includes at least one power module configured to send to each electric motor winding a phase current and at least one control module configured to control, in response to a braking setpoint, the sending by the power module of a setpoint phase current determined depending on the braking force to be applied. The method further includes the variation of the phase current transmitted to each winding of the electric motor so as to cause the phase current to oscillate around the setpoint phase current.
1. A control method for an electrical braking system for aircraft comprising a plurality of electromechanical actuators configured to apply a braking force on friction members, each electromechanical actuator comprising an electric motor equipped with one or more windings, the braking system further comprising at least one power module configured to send to each electric motor winding a phase current and at least one control module configured to control, in response to a braking setpoint received by the at least one control module, the sending by the power module of a setpoint phase current determined depending on the braking force to be applied by the electromechanical actuator, wherein the method comprises the variation of the phase current transmitted to each winding of the electric motor so as to cause said phase current to oscillate around the setpoint phase current.
2. The method according to claim 1 , wherein the braking setpoint comprises a position setpoint of each electromechanical actuator and wherein the variation of the phase current is accomplished by application of an oscillating movement around the position setpoint.
3. The method according to claim 1 , wherein the braking setpoint comprises a force setpoint of each electromechanical actuator and wherein the variation of the phase current is accomplished by application of an oscillating movement around the force setpoint of the actuator.
4. The method according to claim 1 , wherein the variation of the phase current is accomplished by application of a modulation directly to the setpoint phase current.
5. The method according to claim 1 , wherein the variation of the phase current transmitted to each winding of the electric motor is accomplished in response to a detection of a braking setpoint comprising a fixed position setpoint or a constant force setpoint.
6. An electrical braking system for aircraft comprising a plurality of electromechanical actuators configured to apply a braking force on friction members, each electromechanical actuator comprising an electric motor equipped with one or more windings, the braking system further comprising at least one power module configured to send to each electric motor winding a phase current and at least one control module configured to control, in response to a braking setpoint received by the at least one control module, the sending by the power module of a setpoint phase current determined depending on the braking force to be applied by the electromechanical actuator, wherein the system comprises a modulation system configured to cause the phase current transmitted to each winding of the electric motor to vary so as to cause said phase current to oscillate around the setpoint phase current.
7. The system according to claim 6 , wherein the braking setpoint comprises a position setpoint of each electromechanical actuator and wherein the modulation system is configured to apply an oscillating movement around the setpoint position.
8. The system according to claim 6 , wherein the braking setpoint comprises a force setpoint of each electromechanical actuator and wherein the modulation system is configured to apply an oscillating movement around the force setpoint of the actuator.
9. The system according to claim 6 , wherein the modulation system is configured to apply a modulation directly to the setpoint phase current.
10. The system according to claim 6 , wherein the modulation system is configured to cause the phase current transmitted to each winding of the electric motor to vary in response to a detection of a braking setpoint comprising a fixed position setpoint or a constant force setpoint.