A HAPTIC INTERFACE SYSTEM FOR PROVIDING A HAPTIC STIMULUS INDICATIVE OF A VIRTUAL RELIEF

• US 20170160804A1
• Filed: 06/05/2015
• Published: 06/08/2017
• Est. Priority Date: 06/06/2014
• Status: Abandoned Application

• Current Assignee: Fondazione Istituto Italiano di Tecnologia
• Original Assignee: Fondazione Istituto Italiano di Tecnologia
• Inventors: Brayda, Luca, Torazza, Diego, Zini, Giorgio, Sandini, Giulio
• Application Number:
  US15/316,559
• Publication Number:
  US 20170160804A1
• Time in Patent Office: Days
• CPC Class Codes: G06F 2203/015 Force feedback applied to a joystick
• CPC Class Codes: G06F 3/016 Input arrangements with force or tactile feedback as computer generated output to the user
• CPC Class Codes: G06F 3/0338 with detection of limited linear or angular displacement of an operating part of the device from a neutral position, e.g. isotonic or isometric joysticks
• CPC Class Codes: G06F 3/03543 Mice or pucks G06F3/03541 takes precedence

Abstract

A haptic interface system comprising: a shell which is moved on a reference surface by a user; an actuator mechanically coupled to the shell, which provides a haptic stimulus on a fingertip of the user; and a motor assembly, which moves the actuator with three degrees of freedom. The haptic interface system also includes: a localization system, which determines the position and orientation of the shell with respect to the reference surface; and a control stage, which controls the motor assembly so as to move the actuator as a function of the position of the shell, in an invariant manner with respect to the orientation of the shell.

Claims

1. A haptic interface system comprising:

a shell which may be manipulated by a user and is configured to be moved on a reference surface by the user;

an actuator mechanically coupled to the shell and apt to provide a haptic stimulus on a fingertip of the user;

a motor assembly configured to move the actuator with three degrees of freedom;

characterized by;

a localization system configured to determine the position and orientation of the shell with respect to the reference surface; and

a control stage configured to control the motor assembly so as to move the actuator as a function of the position of the shell, in an invariant manner with respect to the orientation of the shell.

2. The system according to claim 1, wherein the shell is integral with a reference system (xyz) comprising a first, a second and a third axis (x, y, z), and wherein the motor assembly is such that the actuator is configured to rotate about axes respectively parallel to the first or the second axis (x, y) and to move parallel to the third axis (z).

3. The system according to claim 1, further comprising a memory unit configured to store a virtual three-dimensional surface;

and wherein the control stage comprises;

a selection unit configured to select a point of the virtual three-dimensional surface, as a function of the position of the shell on the reference surface, the selected virtual point having a respective height, and the virtual three-dimensional surface having a respective inclination at the selected virtual point; and

an actuation unit configured to control the motor assembly so as to;

arrange the actuator at a height, with respect to the reference surface, which is a function of the height of the selected virtual point; and

tilt the actuator with respect to the reference surface, as a function of said respective inclination of the virtual three-dimensional surface.

4. The system according to claim 1, further comprising a first and a second magnetic unit integral with the shell and configured to respectively generate a first and a second magnetic field, said localization system comprising:

a graphics tablet, which forms said reference surface and is configured to generate a preliminary signal indicative of the positions of the first and second magnetic units; and

a computer (104) configured to determine the position and orientation of the shell (2), as a function of the preliminary signal.

5. The system according to claim 1, further comprising a first vibrating motor configured to cause a vibration of the actuator with respect to the shell.

6. The system according to claim 1, further comprising a second vibrating motor configured to cause a vibration of the shell with respect to a support plane, when the shell is arranged on said support plane.

7. The system according to claim 1, further comprising at least a first sensor configured to generate a first force signal, indicative of a force exerted by the user on the actuator.

8. The system according to claim 7, further comprising:

a second and a third sensor configured to respectively generate a second and a third force signal, the first, the second and the third force signals being indicative of the corresponding components directed along different directions of said force exerted by the user.

9. The system according to claim 8, further comprising a processing unit configured to determine the direction along which the user exerts said force on the actuator, on the basis of the first, the second and the third force signals.

10. The system according to claim 1, wherein the motor assembly comprises a first, a second and a third motor and a connection stage, and wherein the connection stage comprises:

a first crank configured to be driven in rotation by the first motor;

a first rod having a first and a second end, the first end of the first rod being hinged to the first crank, the second end of the first rod having the shape of a portion of a sphere and forming a first ball joint with the actuator;

a second crank configured to be driven in rotation by the second motor;

a second rod having a first and a second end, the first end of the second rod being hinged to the second crank, the second end of the second rod having the shape of a portion of a sphere and forming a second ball joint with the actuator;

a third crank configured to be driven in rotation by the third motor;

a third rod having a first and a second end, the first end of the third rod being hinged to the third crank, the second end of the third rod having the shape of a portion of a sphere and forming a third ball joint with the actuator.

11. The system according to claim 8, wherein the first, the second and the third sensor are respectively formed by a first, a second and a third strain gauge, wherein the motor assembly comprises a first, a second and a third motor and a connection stage, and wherein the connection stage comprises:

a first crank configured to be driven in rotation by the first motor;

a first rod having a first and a second end, the first end of the first rod being hinged to the first crank, the second end of the first rod having the shape of a portion of a sphere and forming a first ball joint with the actuator;

a second crank configured to be driven in rotation by the second motor;

a second rod having a first and a second end, the first end of the second rod being hinged to the second crank, the second end of the second rod having the shape of a portion of a sphere and forming a second ball joint with the actuator;

a third crank configured to be driven in rotation by the third motor;

a third rod having a first and a second end, the first end of the third rod being hinged to the third crank, the second end of the third rod having the shape of a portion of a sphere and forming a third ball joint with the actuator; and

wherein said first, second and third strain gauges are mechanically coupled to the first, the second and the third rod, respectively.