System and method for tactile cueing through rotorcraft pilot controls using variable friction and force gradient

Patent metadata

Field	Value
Publication number	US-11117653-B2
Application number	US-201815983752-A
Country	US
Kind code	B2
Filing date	May 18, 2018
Priority date	Nov 28, 2017
Publication date	Sep 14, 2021
Grant date	Sep 14, 2021

Abstract

An rotorcraft including a pilot control, a pilot control position sensor connected to the pilot control and operable to generate a position signal indicating a position of the pilot control, a flight control computer (FCC) in signal communication with the pilot control position sensor and operable to provide a tactile cue in the pilot control in response to the position signal indicating the position of the pilot control exceeds a threshold associated with an operating limit, and further operable to determine a tactile cueing value for the tactile cue according to a relationship between the position of the pilot control and the threshold, and generate a cue control signal according to the tactile cueing value, and a tactile cue element connected to the pilot control and in signal communication with the FCC and operable to control action of the pilot control in response to the cue control signal.

First claim

What is claimed is:

1. A rotorcraft, comprising:
a pilot collective control;
a pilot control position sensor connected to the pilot collective control, wherein the pilot control position sensor is operable to generate a position signal indicating a position of the pilot collective control;
a flight control computer (FCC) in signal communication with the pilot control position sensor and operable to provide tactile cues in the pilot collective control in response to the position signal indicating the position of the pilot collective control has exceeded a threshold associated with an operating limit, wherein the tactile cues comprise a friction cue and a force cue, wherein the FCC is further operable to determine tactile cueing values for the tactile cues according to a relationship between the position of the pilot collective control and the threshold, and generate cue control signals according to the tactile cueing values; and
tactile cue elements connected to the pilot collective control and in signal communication with the FCC, wherein the tactile cue elements are operable to control action of the pilot collective control in response to the cue control signals;
wherein the tactile cue elements comprise a friction device connected to a variable coupling disposed between the friction device and the pilot collective control, and wherein the friction device provides the friction cue through the variable coupling to the pilot collective control in response to the cue control signals;
wherein the tactile cue elements further comprise a trim motor connected to the variable coupling separately from the friction device, wherein the variable coupling is disposed between the pilot collective control and the trim motor, and wherein the trim motor provides the force cue, separate from the friction cue, through the variable coupling to the pilot collective control in response to the cue control signals.

2. The rotorcraft of claim 1 , wherein the tactile cueing values are magnitudes of the tactile cues.

3. The rotorcraft of claim 2 , wherein the friction cue is a variable friction cue and wherein the friction device is operable to control action of the pilot collective control to implement the variable friction cue by providing a force that is resistant to movement of the pilot collective control.

4. The rotorcraft of claim 2 , wherein the force cue is a gradient force cue and wherein the trim motor is operable to control action of the pilot collective control to implement the gradient force cue by providing a force on the pilot collective control that pushes the pilot collective control toward the threshold.

5. The rotorcraft of claim 1 , wherein the friction cue is a variable friction cue and wherein the force cue is a gradient force cue.

6. The rotorcraft of claim 5 , wherein the FCC is operable determine a friction cue limit and a force cue limit according to the operating limit;
wherein the FCC is further operable to determine a friction cueing value according to a relationship between the position of the pilot collective control and the friction cue limit and generate a friction cue control signal according to the friction cueing value;
wherein the FCC being operable to determine the tactile cueing values comprises the FCC being operable to determine a force cueing value according to the relationship between the position of the pilot collective control and the force cue limit and further operable to generate a force cue control signal according to the force cueing value;
wherein the friction device is further operable to provide the friction cue, which is resistant to movement of the pilot collective control, according to the friction cue control signal; and
wherein the trim motor is further operable to provide the force cue on the pilot collective control in a direction of the threshold according to the force cue control signal.

7. The rotorcraft of claim 1 , wherein the variable coupling is a planetary gear set transmission connecting the friction device and the trim motor to the pilot collective control.

8. A flight control computer (FCC) for a rotorcraft, comprising:
a processor; and
a non-transitory computer-readable storage medium storing a program to be executed by the processor, the program including instructions for providing tactile cues, the instructions for providing the tactile cues including instructions for:
receiving a position signal indicating a position of a collective control of the rotorcraft;
determining cue limits according to one or more operating limits of the rotorcraft, wherein the cue limits comprise a friction cue limit and a force cue limit;
determining to apply the tactile cues according to a relationship between the respective cue limits and the position of the collective control; and
controlling action of the collective control in response to determining to apply the tactile cues and using a magnitude of the tactile cues determined according to the relationship between the respective cue limits and the position of the collective control;

wherein the instructions for controlling the action of the collective control include instructions for controlling, according to the friction cue limit, a friction device connected to a variable coupling disposed between the friction device and the collective control, wherein the controlling the friction device provides a friction cue through the variable coupling to the collective control;
wherein the instructions for controlling the action of the collective control further include instructions for controlling, according to the force cue limit and separately from controlling the friction device, a trim motor connected to the variable coupling separately from the friction device, wherein the variable coupling is disposed between the collective control and the trim motor, wherein the controlling the trim motor provides a force cue, separate from the friction cue, through the variable coupling to the collective control.

9. The FCC of claim 8 , wherein the instructions for determining the magnitude of the tactile cues include instructions for:
using a sum of a predetermined step change cueing value and a gradient cue value as the magnitude of the respective tactile cues, wherein the predetermined step change cueing value is a constant, and wherein the gradient cue value is determined according to a distance which the position of the collective control exceeds the respective cue limits.

10. The FCC of claim 8 , wherein the one or more operating limits include an engine limit selected from a plurality of engine power settings.

11. The FCC of claim 10 , wherein the instructions for determining the cue limits include instructions for determining the friction cue limit and the force cue limit according to the one or more operating limits;
wherein the instructions for determining the magnitude of the tactile cues include instructions for determining a friction cueing value associated with the friction cue according to a relationship between the position of the collective control and the friction cue limit; and
wherein the instructions for determining the magnitude of the tactile cues further include instructions for determining a force cueing value associated with the force cue according to the relationship between the position of the collective control and the force cue limit.

12. The FCC of claim 11 , wherein the friction cue limit is different from the force cue limit.

13. A method for operating a rotorcraft, comprising:
providing tactile cues on a collective control of the rotorcraft by performing:
receiving a position signal indicating a position of the collective control;
determini

Assignees

• Textron Innovations Inc

Inventors

• Covington Charles Eric
• Linton Bradley Don
• Johnson Jr Thomas Earl
• Dafydd Gillett Luke
• Worsham Ii Robert Earl
• Alfred Jillian Samantha

Classifications

• G05G5/03

  Means for enhancing the operator's awareness of arrival of the controlling member at a command or datum position; Providing feel, e.g. means for creating a counterforce (arrangements for indicating the position of the controlling member G05G1/015) · CPC title

• B64C27/56 Primary

  characterised by the control initiating means, e.g. manually actuated · CPC title

• B64D47/00

  Equipment not otherwise provided for · CPC title

• B64D43/00

  Arrangements or adaptations of instruments · CPC title

• B64C27/57

  automatic or condition responsive, e.g. responsive to rotor speed, torque or thrust · CPC title