Force feedback fault detection and accommodation for a multi-channel electric brake actuator controller

Patent metadata

Field	Value
Publication number	US-10427665-B2
Application number	US-201615075956-A
Country	US
Kind code	B2
Filing date	Mar 21, 2016
Priority date	Mar 21, 2016
Publication date	Oct 1, 2019
Grant date	Oct 1, 2019

Abstract

A method for fault detection and accommodation for a controller and actuator system is provided. The method includes receiving, from a controller, a flag at an actuator in response to an excitation voltage and current falling below a threshold value, engaging a sensor in the actuator in response to receiving the flag, receiving, using the sensor a first load cell signal and a second load cell signal in response to the sensor being engaged, determining how actuator is operating brake based on the received flag, first load cell signal, and second load cell signal, adjusting a state of the actuator based on the determination, and reporting the state of the actuator by transmitting a report signal to the controller.

First claim

What is claimed is:

1. A method of fault detection and accommodation for a controller and actuator system, wherein the actuator system includes an actuator and having a sensor and controls operation of an electric brake, the method comprising:
generating and transmitting from the controller to the actuator a controller excitation current;
receiving at the controller a signal from the actuator system, the signal including a measured excitation current measured by the sensor;
setting a flag in the controller in response to the measured excitation current falling below a threshold value;
transmitting a flag signal after the flag is set, the flag signal being transmitted from the controller to control circuitry on the actuator;
receiving from the electric brake at the control circuitry on the actuator a first and second load cell signals that are based on a braking force applied by the electric brake;
determining at the control circuitry on the actuator how the actuator is operating the electric brake based on the first and second load signals wherein determining includes comparing the first and second load cell signals to expected first and second load cell signals;
adjusting a state of the actuator based on determining how the actuator is operating and transmitting the state to the controller;
adjust a state of the actuator in the controller based on the determination, wherein adjusting the state includes calculating a gain correction to be applied to the controller excitation current to reduce a force error of the actuator; and
operating the controller with the corrected gain.

2. The method of claim 1 ,
wherein the controller is an electric brake actuator controller (EBAC),
wherein the actuator is an electric brake actuator (EBA),
wherein the EBAC is connected to the actuator through a harnessing, and
wherein the harnessing comprises a wire harness, a junction box, and a wire bundle assembly (WBA).

3. The method of claim 1 ,
wherein the controller and actuator system comprises a plurality of actuators connected to the controller.

Assignees

• Simmonds Precision Products

Inventors

• Mastrocola Naison E
• Abbott Michael
• Richardson Brian L

Classifications

• B60T8/1703 Primary

  for aircrafts · CPC title

• B60T8/325

  Systems specially adapted for aircraft · CPC title

• B60T2270/403

  Brake circuit failure · CPC title

• B60T17/221 Primary

  Procedure or apparatus for checking or keeping in a correct functioning condition of brake systems (hydraulic pressure systems in general F15B19/00, F15B21/04; testing structures or apparatus G01M) · CPC title