Inceptor and method for operating an inceptor

• US 9,969,485 B2
• Filed: 06/27/2014
• Issued: 05/15/2018
• Est. Priority Date: 07/01/2013
• Status: Active Grant

• Current Assignee: BAE Systems Plc
• Original Assignee: BAE Systems Plc
• Inventors: Davies, Robin William
• Primary Examiner(s): Black, Thomas G
• Assistant Examiner(s): LOUIE, WAE LENNY
• Application Number:
  US14/901,747
• Publication Number:
  US 20160355251A1
• Time in Patent Office: 1,418 Days
• Field of Search: 701 3, 701301, 244221, 244223
• CPC Class Codes: B64C 13/0421 control sticks for primary flight controls
• CPC Class Codes: B64C 13/22 readily revertible to personal control

Abstract

An inceptor apparatus (10) for controlling a vehicle, in particular an aircraft comprises a control stick (15) for operation by a user and a user feedback generator (28) coupled to the control stick and configured to receive signals from a vehicle condition indicator (40) remote from the inceptor apparatus. The apparatus also has a first vehicle condition sensor (54,56) dedicated to the operation of the inceptor apparatus. In a first mode of operation, the user feedback generator (28) is operable to generate tactile feedback to the user via the control stick in dependence upon signals received from the vehicle condition indicator (40). In a second mode of operation, in the event that no signal is received from the vehicle condition indicator (40), the user feedback generator (28) is operable to generate tactile feedback to the user via the control stick in dependence upon signals received from the first vehicle condition sensor (54,56).

Claims

1. An inceptor apparatus for controlling a vehicle, comprising:

a control stick for operation by a user;

a user feedback generator coupled to the control stick and configured to receive signals from a vehicle condition indicator remote from the inceptor apparatus, the signals from the vehicle condition indicator representing a condition of the vehicle; and

a first vehicle condition sensor dedicated to the operation of the inceptor apparatus;

wherein in a first mode of operation, in the event that the signals are received from the vehicle condition indicator, the user feedback generator is operable to generate tactile feedback to the user via the control stick in dependence upon the signals received from the vehicle condition indicator; and

wherein in a second mode of operation, in the event that no signal is received from the vehicle condition indicator, the user feedback generator is operable to generate tactile feedback to the user via the control stick in dependence upon signals received from the first vehicle condition sensor.

2. The inceptor apparatus as claimed in claim 1 wherein, in a third mode of operation, the user feedback generator provides no feedback to the user.

3. The inceptor apparatus as claimed in claim 1, wherein the first and second modes of operation each correspond to a vehicle condition which requires the user'"'"'s input.

4. The inceptor apparatus as claimed in claim 2, wherein the third mode of operation corresponds to a vehicle condition in which the vehicle is being computer operated without the need for user intervention.

5. The inceptor apparatus as claimed in claim 1, wherein the first vehicle condition sensor is configured to generate and deliver a signal indicative of at least one of vehicle attitude and vehicle speed.

6. The inceptor apparatus as claimed in claim 1, wherein, in the second mode of operation, the user feedback generator generates tactile feedback to the user via the control stick in dependence also upon signals received from a second vehicle condition sensor, wherein the first vehicle condition sensor is configured to generate a signal indicative of vehicle attitude and the second vehicle condition sensor is configured to generate and deliver a signal indicative of vehicle speed.

7. A vehicle control system comprising an inceptor apparatus as claimed in claim 1.

8. The vehicle control system as claimed in claim 7, wherein the vehicle is an aircraft, and wherein the vehicle condition indicator is a flight control computer (FCC) configured to generate a signal indicative of at least one of vehicle attitude and vehicle speed for the operation of the aircraft.

9. A method of operating an inceptor apparatus for a vehicle, the method comprising:

determining if the vehicle is operating normally;

in the event that signals are received from a vehicle condition indicator remote from the interceptor apparatus, providing tactile feedback to the user via a control stick coupled to a user feedback generator in dependence upon the signals received from a vehicle condition indicator, the signals from the vehicle condition indicator representing a condition of the vehicle; and

in the event that no signal is received from the vehicle condition indicator, providing tactile feedback to the user via the control stick coupled to the user feedback generator in dependence upon signals from a vehicle condition sensor dedicated to the inceptor apparatus.

10. The method as claimed in claim 9, further comprising:

in response to the vehicle being computer operated without the need for user intervention, providing no tactile feedback to the user via the control stick coupled to the user feedback generator.

11. The method as claimed in claim 9, further comprising:

providing tactile feedback to the user via the control stick coupled to the user feedback generator in dependence upon signals from a second vehicle condition sensor;

wherein the first vehicle condition sensor is configured to generate a signal indicative of one of vehicle attitude or vehicle speed, and the second vehicle condition sensor is configured to generate and deliver a signal indicative of the other one of vehicle attitude or vehicle speed.

12. The method as claimed in claim 9, wherein the vehicle is an aircraft, and the vehicle condition indicator is a flight control computer (FCC) configured to generate a signal indicative of at least one of vehicle attitude and vehicle speed for the operation of the aircraft.

13. An inceptor apparatus for controlling an aircraft, comprising:

a user control stick;

a first vehicle condition sensor; and

a user feedback generator coupled to the control stick and including an actuator, wherein;

in a first mode of operation, in the event that signals are received from an aircraft condition indicator remote from the inceptor apparatus, the user feedback generator is operable to generate tactile feedback via the control stick in dependence upon the signals received from the aircraft condition indicator, the signals from the aircraft condition indicator representing a condition of the aircraft; and

in a second mode of operation, in the event that no signal is received from the aircraft condition indicator, the user feedback generator is operable to generate tactile feedback via the control stick in dependence upon signals received from the first vehicle condition sensor.

14. The inceptor apparatus as claimed in claim 13, wherein, in a third mode of operation, the user feedback generator provides no feedback, wherein the third mode of operation corresponds to an aircraft condition in which the aircraft is being computer operated without the need for user intervention.

15. The inceptor apparatus as claimed in claim 13, wherein the first and second modes of operation correspond to an aircraft condition which requires pilot input.

16. The inceptor apparatus as claimed in claim 13, wherein the first vehicle condition sensor is configured to generate and deliver a signal indicative of at least one of aircraft attitude and aircraft speed.

17. The inceptor apparatus as claimed in claim 13, wherein, in the second mode of operation, the user feedback generator generates tactile feedback to the user via the control stick in dependence also upon signals received from a second vehicle condition sensor, wherein the first vehicle condition sensor is configured to generate a signal indicative of one of aircraft attitude or aircraft speed, and the second vehicle condition sensor is configured to generate and deliver a signal indicative of the other one of aircraft attitude or aircraft speed.

18. An aircraft control system comprising an inceptor apparatus as claimed in claim 13.

19. The aircraft control system as claimed in claim 18, wherein the aircraft condition indicator is a flight control computer (FCC) configured to generate a signal indicative of at least one of aircraft attitude and aircraft speed for the operation of the aircraft.

20. The aircraft control system as claimed in claim 18, wherein the flight control computer (FCC) is further configured to receive data from one or more additional sensors.