Pilot flight control stick feedback system

• US 20070235594A1
• Filed: 04/06/2006
• Published: 10/11/2007
• Est. Priority Date: 04/06/2006
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Hanlon, Casey, Wingett, Paul, Potter, Calvin
• Application Number:
  US11/400,251
• Publication Number:
  US 20070235594A1
• Time in Patent Office: Days
• US Class Current: 244/223
• CPC Class Codes: B64C 13/02 Initiating means
• CPC Class Codes: B64C 13/345 with artificial feel
• CPC Class Codes: B64C 13/507 with artificial feel
• CPC Class Codes: G05G 2009/04707 with ball joint
• CPC Class Codes: G05G 2009/04766 providing feel, e.g. indexing means, means to create counterforce
• CPC Class Codes: G05G 9/047 the controlling member being movable by hand about orthogonal axes, e.g. joysticks for switches H01H25/04

Abstract

A pilot flight control stick haptic feedback mechanism provides variable force feedback to the pilot flight control stick based on actual aircraft conditions. The flight control stick is movable to a control position in a displacement direction. A control unit receives one or more signals representative of aircraft conditions and, in response thereto, selectively supplies a variable force feedback signal. A magnetic bearing is disposed adjacent at least a portion of the flight control stick, and is responsive to the variable force feedback signal to supply a variable magnetic feedback force to the flight control stick in a direction that opposes the displacement direction.

Claims

1. An aircraft flight control surface actuation haptic feedback system, comprising:

a flight control stick adapted to receive an input force supplied by a pilot and configured, upon receipt of the input force, to move to a control position in a displacement direction;

a control unit adapted to receive signals representative of aircraft speed, aircraft altitude, aircraft attitude, and aircraft flight envelope and operable, in response thereto, to supply a plurality of independent variable force feedback signals; and

a magnetic bearing including a rotor and a plurality of stators, the magnetic bearing rotor coupled to the flight control stick, each magnetic bearing stator disposed adjacent to, and spaced apart from, the magnetic bearing rotor, each magnetic bearing stator coupled to receive one of the independent variable force feedback signals and operable, in response thereto, to supply a variable magnetic feedback force to the magnetic bearing rotor that urges the magnetic bearing rotor in a direction that opposes the displacement direction of the flight control stick.

2. The system of claim 1, wherein:

the flight control stick is further configured, upon movement thereof to the control position, to supply a flight control surface position control signal based at least in part on the control position; and

the control unit is coupled to receive the flight control surface position control signal from the flight control stick and is further operable, in response thereto, to supply one or more flight control surface position commands.

3. The system of claim 2, further comprising:

one or more flight control stick position sensors configured to sense the control position of the flight control stick and operable to supply the flight control surface position control signal.

4. The system of claim 2, wherein the control unit is further responsive to the flight control surface position control signal to supply the plurality of independent variable force feedback signals.

5. The system of claim 1, wherein the control unit is further adapted to receive signals representative of aircraft flight control surface positions.

7. The system of claim 1, further comprising:

a second flight control stick adapted to receive an input force supplied by a second pilot and configured, upon receipt of the input force, to (i) move to a control position in a displacement direction and (ii) supply a flight control surface position control signal based at least in part on the control position,

wherein the control unit is coupled to receive the flight control surface position control signal from the second flight control stick and is further operable, in response thereto, to supply the plurality of independent variable force feedback signals.

6. (canceled)

8-10. -10. (canceled)

11. An aircraft flight control surface actuation system, comprising:

a flight control stick adapted to receive an input force supplied by a pilot and configured, upon receipt of the input force, to (i) move to a control position in a displacement direction and (ii) supply a flight control surface position control signal based at least in part on the control position to which the flight control stick is moved;

a control unit coupled to receive (i) the flight control surface position control signal and (ii) signals representative of aircraft speed, aircraft altitude aircraft attitude and aircraft flight envelope and operable, in response thereto, to (i) supply one or more flight control surface position commands and (ii) supply a plurality of independent variable force feedback signals; and

a magnetic bearing including a rotor and a plurality of stators, the magnetic bearing rotor coupled to the flight control stick, each magnetic bearing stator disposed adjacent to, and spaced apart from, the magnetic bearing rotor, each magnetic bearing stator coupled to receive one of the independent variable force feedback signals and operable, in response thereto, to supply a variable magnetic feedback force to the magnetic bearing rotor that urges the magnetic bearing rotor in a direction that opposes the displacement direction of the flight control stick.

12. The system of claim 11, further comprising:

one or more flight control stick position sensors configured to sense the control position of the flight control stick and operable to supply the flight control surface position control signal.

13. The system of claim 12, wherein the control unit is further responsive to the flight control surface position control signal to supply the plurality of independent variable force feedback signals.

14. The system of claim 11, wherein the one or more signals representative of aircraft flight conditions include one or more signals representative of aircraft flight control surface positions.

16. The system of claim 11, further comprising:

a second flight control stick adapted to receive an input force supplied by a second pilot and configured, upon receipt of the input force, to (i) move at least a portion thereof to a control position in a displacement direction and (ii) supply a flight control surface position control signal based at least in part on the control position,

wherein the control unit is coupled to receive the flight control surface position control signal from the second flight control stick and is further operable, in response thereto, to supply the plurality of independent variable force feedback signals.

15. (canceled)

17-18. -18. (canceled)

19. An aircraft flight control surface actuation system, comprising:

a flight control stick adapted to receive an input force supplied by a pilot and configured, upon receipt of the input force, to move to a control position in a displacement direction

one or more flight control stick position sensors configured to sense the control position of the flight control stick and operable to supply a flight control surface position control signal based at least in part on the sensed control position;

a control unit coupled to receive (i) the flight control surface position control signal, (ii) one or more signals representative of aircraft conditions, and (iii) a signal representative of aircraft operational envelope, and operable, in response thereto, to (i) supply one or more flight control surface position commands and (ii) supply a plurality of independent variable force feedback signals; and

a magnetic bearing including a rotor and a plurality of stators, the magnetic bearing rotor coupled to the flight control stick, each magnetic bearing stator disposed adjacent to, and spaced apart from, the magnetic bearing rotor, each magnetic bearing stator coupled to receive one of the independent variable force feedback signals and operable, in response thereto, to supply a variable magnetic feedback force to the magnetic bearing rotor that urges the magnetic bearing rotor in a direction that opposes the displacement direction of the flight control stick.

20. (canceled)