Brake force measurement techniques

Patent metadata

Field	Value
Publication number	US-9533666-B2
Application number	US-201514671642-A
Country	US
Kind code	B2
Filing date	Mar 27, 2015
Priority date	Mar 27, 2015
Publication date	Jan 3, 2017
Grant date	Jan 3, 2017

Abstract

The present disclosure provides systems and methods related to determining observed applied brake force of an aircraft braking system. In various embodiments, a system for calculating observed applied force comprises a current sensor in communication with a controller, a position sensor in communication with the controller and configured to measure a rotational speed of a motor shaft, and a tangible, non-transitory memory configured to communicate with the controller. In various embodiments, the tangible, non-transitory memory may have instructions stored thereon that, in response to execution by the controller, cause the controller to perform operations comprising receiving, by the controller, a motor current from the current sensor at a first time, calculating, by the controller, a first electromagnetic torque, calculating, by the controller, a first flywheel angular velocity, receiving, by the controller, a motor shaft angular velocity from the position sensor at a second time, subtracting, by the controller, the first flywheel angular velocity and the motor shaft angular velocity received at the second time to obtain a first angular velocity difference, calculating, by the controller, a first observed disturbance torque, and calculating, by the controller, a first observed applied force.

First claim

What is claimed is:

1. A system for calculating observed applied force, comprising:
a current sensor, in communication with a controller;
a position sensor, in communication with the controller and configured to measure a rotational speed of a motor shaft; and
a tangible, non-transitory memory configured to communicate with the controller, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the controller, cause the controller to perform operations comprising:
receiving, by the controller, a motor current from the current sensor at a first time;
calculating, by the controller, a first electromagnetic torque;
calculating, by the controller, a first flywheel angular velocity;
receiving, by the controller, a motor shaft angular velocity from the position sensor at a second time;
subtracting, by the controller, the first flywheel angular velocity and the motor shaft angular velocity received at the second time to obtain a first angular velocity difference;
calculating, by the controller, a first observed disturbance torque; and
calculating, by the controller, a first observed applied force.

2. The system of claim 1 , wherein the controller uses the first observed disturbance torque, a gear ratio factor, a ball screw lead angle factor, and a transmission efficiency factor to calculate the first observed applied force.

3. The system of claim 1 , wherein the operations further comprise:
comparing the first observed applied force to a commanded force.

4. The system of claim 1 , wherein the instructions cause the controller to perform the operations further comprising:
receiving, by the controller, a motor current from the current sensor at a third time;
calculating, by the controller, a second electromagnetic torque;
subtracting, by the controller, the first observed disturbance torque and the second electromagnetic torque to obtain an effective torque;
calculating, by the controller, a second flywheel angular velocity;
receiving, by the controller, a motor shaft angular velocity from the position sensor at a fourth time;
subtracting, by the controller, the second flywheel angular velocity and the motor shaft angular velocity received at the fourth time to obtain a second angular velocity difference;
calculating, by the controller, a second observed disturbance torque; and
calculating, by the controller, a second observed applied force.

5. The system of claim 4 , wherein the instructions cause the controller to perform the operations further comprising:
comparing the second observed applied force to a commanded force.

6. The system of claim 5 , wherein the instructions cause the controller to perform the operations further comprising:
repeating the receiving the motor current at the third time, the calculating the electromagnetic torque, the subtracting the first observed disturbance torque and the second electromagnetic torque, the calculating the second flywheel angular velocity, the receiving the motor shaft angular velocity at the fourth time, the subtracting the second flywheel angular velocity received at the fourth time and the second motor shaft angular velocity, the calculating the second observed disturbance torque, the calculating the second observed applied force, and the comparing the second observed applied force to the commanded force.

7. The system of claim 4 , wherein the position sensor comprises at least one of a resolver and a tachometer.

8. The system of claim 4 , wherein the controller comprises an electromechanical motor actuator controller.

9. The system of claim 4 , wherein the controller comprises an electromechanical brake controller unit.

10. A method for determining an observed applied force, comprising:
Measuring, by a current sensor in communication with a controller, a motor current at a first time;
Calculating, by the controller, a first electromagnetic torque;
Calculating, by the controller, a first flywheel angular velocity;
measuring, by a position sensor in communication with the controller, a motor shaft angular velocity at a second time;
subtracting, by the controller, the first flywheel angular velocity and the motor shaft angular velocity measured at the second time to obtain a first angular velocity difference;
calculating, by the controller, a first observed disturbance torque; and
calculating, by the controller, a first observed applied force.

11. The method of claim 10 , wherein the first observed disturbance torque, a gear ratio factor, a ball screw lead angle factor, and a transmission efficiency factor are used to calculate the first observed applied force.

12. The method of claim 10 , further comprising:
comparing, by the controller, the first observed applied force to a commanded force.

13. The method of claim 10 , further comprising:
Measuring, by the current sensor, a motor current at a third time;
calculating, by the controller, a second electromagnetic torque;
subtracting, by the controller, the first observed disturbance torque and the second electromagnetic torque to obtain a first effective torque;
calculating, by the controller, a second flywheel angular velocity;
measuring, by the position sensor, a motor shaft angular velocity at a fourth time;
subtracting, by the controller, the second flywheel angular velocity and the motor shaft angular velocity measured at the fourth time to obtain a second angular velocity difference;
calculating, by the controller, a second observed disturbance torque; and
calculating, by the controller, a second observed applied force.

14. The method of claim 13 , further comprising:
comparing, by the controller, the second observed applied force to a commanded force.

15. The method of claim 14 , further comprising:
repeating, as needed, the measuring the motor current, the calculating the second electromagnetic torque, the subtracting the first observed disturbance torque and the second electromagnetic torque, the calculating the second flywheel angular velocity, the measuring the motor shaft angular velocity at the fourth time, the subtracting the second flywheel angular velocity and the motor shaft angular velocity measured at the fourth time, the calculating the second observed disturbance torque, the calculating the second observed applied force, and the comparing the second observed applied force to the commanded force.

Assignees

• Goodrich Corp

Inventors

• Ayichew Efrem E
• Kolk Richard

Classifications

• B60T17/22 Primary

  Devices for monitoring or checking brake systems; Signal devices · CPC title

• B60T8/171

  Detecting parameters used in the regulation; Measuring values used in the regulation · CPC title

• B60T8/1703 Primary

  for aircrafts · CPC title