Systems and methods for controlling a resistive force of an inceptor of an aircraft

Patent metadata

Field	Value
Publication number	US-11745856-B2
Application number	US-202017132555-A
Country	US
Kind code	B2
Filing date	Dec 23, 2020
Priority date	Dec 30, 2019
Publication date	Sep 5, 2023
Grant date	Sep 5, 2023

Abstract

Methods and systems for adjusting a force feel profile of an inceptor of an aircraft are provided. The force feel profile is based on a baseline value of an operating parameter of the aircraft and defines an amount of resistive force applied to the inceptor as a function of displacement of the inceptor. An embodiment of the method includes receiving data indicative of a current value of the operating parameter. Based on a difference between the current value and the baseline value of the operating parameter, a portion of the force feel profile corresponding to a range of displacement values is shifted to adjust an amount of resistive force defined by the portion of the force feel profile for the range of displacement values.

First claim

What is claimed is:

1. A method of controlling a resistive force of an inceptor of an aircraft according to a force feel profile based on a baseline value of an operating parameter of the aircraft and defining an amount of resistive force applied to the inceptor as a function of displacement of the inceptor, the method comprising:
receiving data indicative of a current value of the operating parameter, wherein the operating parameter is a first operating parameter, the force feel profile is based on a baseline value of a second operating parameter of the aircraft, and the first operating parameter is different from the second operating parameter;
receiving data indicative of a current value of the second operating parameter of the aircraft; and
based on a difference between the current and baseline values of the first and second operating parameters, shifting a portion of the force feel profile corresponding to a range of displacement values to adjust the amount of resistive force defined by the portion of the force feel profile for the range of displacement values, wherein the portion of the force feel profile is shifted by an adjustment amount, the adjustment amount is determined using;
a product of a first constant and the difference between the current and baseline values of the first operating parameter; and
a product of a second constant and a difference between the current and baseline values of the second operating parameter, the first constant being different from the second constant;

controlling the resistive force of the inceptor according to the force feel profile including the shifted portion.

2. The method of claim 1 , wherein the operating parameter is indicative of an inertial parameter of the aircraft.

3. The method of claim 1 , wherein the operating parameter is indicative of an acceleration.

4. The method of claim 1 , wherein the operating parameter is indicative of a load on a flight control surface of the aircraft.

5. The method of claim 1 , wherein a gradient of the portion of the force feel profile is unchanged based on the difference between the current and baseline values of the operating parameter.

6. The method of claim 1 , wherein:
the force feel profile defines a soft stop at a soft stop displacement value; and
the soft stop displacement value is unchanged based on the difference between the current and baseline values of the operating parameter.

7. The method of claim 1 , wherein the portion of the force feel profile is shifted within a prescribed boundary.

8. The method of claim 1 , wherein the portion of the force feel profile is shifted by an adjustment amount determined using a product of a constant and the difference between the current and baseline values of the operating parameter.

9. The method of claim 1 , wherein:
the portion of the force feel profile is a first portion of the force feel profile;
the range of displacement values is a first range of displacement values;
the force feel profile includes a second portion corresponding to a second range of displacement values greater than the first range of displacement values; and
the method includes leaving the second portion of the force feel profile unchanged based on the difference between the current and baseline values of the operating parameter.

10. The method of claim 1 , wherein:
the portion of the force feel profile is a first portion of the force feel profile;
the range of displacement values is a first range of displacement values;
the force feel profile includes a second portion corresponding to a second range of displacement values greater than the first range of displacement values; and
the method includes shifting the second portion of the force feel profile based on the difference between the current and baseline values of the operating parameter to adjust an amount of resistive force defined by the second portion of the force feel profile for the second range of displacement values.

11. A system for controlling a resistive force of an inceptor of an aircraft according to a force feel profile based on a baseline value of an operating parameter of the aircraft and defining an amount of resistive force applied to the inceptor as a function of displacement of the inceptor, the system comprising:
one or more data processors operatively coupled to an actuator configured to apply the resistive force to the inceptor; and
non-transitory machine-readable memory storing instructions executable by the one or more data processors and configured to cause the one or more data processors to:
receive data indicative of a current value of the operating parameter, wherein the operating parameter is a first operating parameter, the force feel profile is based on a baseline value of a second operating parameter of the aircraft, and the first operating parameter is different from the second operating parameter;
receiving data indicative of a current value of the second operating parameter of the aircraft; and
generate an output configured to cause the actuator to apply the resistive force to the inceptor according to the force feel profile including a portion shifted to adjust an amount of resistive force defined by the portion for a range of displacement values based on a difference between the current and baseline values of the first and second operating parameters, wherein the portion of the force feel profile is shifted by an adjustment amount, the adjustment amount determined using: a product of a first constant and the difference between the current and baseline values of the first operating parameter; and a product of a second constant and a difference between the current and baseline values of the second operating parameter, the first constant being different from the second constant.

12. The system of claim 11 , wherein the operating parameter is indicative of an inertial parameter of the aircraft.

13. The system of claim 11 , wherein the operating parameter is indicative of an acceleration.

14. The system of claim 11 , wherein the operating parameter is indicative of a load on a flight control surface of the aircraft.

15. The system of claim 11 , wherein a gradient of the portion of the force feel profile is unchanged based on the difference between the current and baseline values of the operating parameter.

16. The system of claim 11 , wherein:
the force feel profile defines a soft stop at a soft stop displacement value; and
the soft stop displacement value is unchanged based on the difference between the current and baseline values of the operating parameter.

17. A method of controlling a resistive force of an inceptor of an aircraft according to a force feel profile defined as a two-dimensional graph having a first axis representing displacement values for the inceptor and a second axis representing corresponding resistive force values applied to the inceptor, the force feel profile being based on a baseline value of an operating parameter of the aircraft, the method comprising:
receiving a current value of the operating parameter, wherein the operating parameter is a first operating parameter, the force feel profile is based on a baseline value of a second operating parameter of the aircraft, and the first operating parameter is different from the second operating parameter;
receiving a current value of the second operating parameter of the aircraft;
based on a difference between the current and baseline values of the first and second operating parameters, shifting a portion of the baseline force feel profile along the second axis by an adjustment amount

Assignees

• Bombardier Inc

Inventors

• Liscouet Jonathan

Classifications

• B64C13/04 Primary

  actuated personally · CPC title

• B64C13/46

  with artificial feel · CPC title

• B64C13/0421

  control sticks for primary flight controls · CPC title

• B64C13/50 Primary

  using electrical energy · CPC title