A vertical gyroscope is adapted for use as a pointing device for controlling the position of a cursor on the display of a computer. A motor at the core of the gyroscope is suspended by two pairs of orthogonal gimbals from a hand-held controller device and nominally oriented with its spin axis vertical by a pendulous device. Electro-optical shaft angle encoders sense the orientation of a hand-held controller device as it is manipulated by a user and the resulting electrical output is converted into a format usable by a computer to control the movement of a cursor on the screen of the computer display. For additional ease of use, the bottom of the controller is rounded so that the controller can be pointing while sitting on a surface. A third input is provided by providing a horizontal gyroscope within the pointing device. The third rotational signal can be used to either rotate a displayed object or to display or simulate a third dimension.

Patent
   RE41520
Priority
Mar 21 1990
Filed
Oct 12 2000
Issued
Aug 17 2010
Expiry
Mar 21 2010
Assg.orig
Entity
Large
0
20
all paid
0. 38. An input device for producing a signal to effect translational movements of a displayable object on a computer graphic display, comprising:
an inertial gyroscopic means adapted for manual movement in free space for producing a signal substantially proportional to rotation of the housing about an axis to effect translational movements of the displayable object on the computer graphic display in substantially continuous proportionality to the signal and in a single direction for each direction in which the inertial gyroscopic means is rotated.
0. 29. An input device for manipulating translational movements of a displayable object on a computer graphic display, comprising:
a hand-held housing adapted for manual movement in free space;
sensing apparatus in the housing to detect gravitational orientation; and
an inertial element mounted with respect to said housing and responsive to rotation of the housing about an axis relative to gravitational orientation for producing a signal indicative of said rotation for manipulating translational movements of the displayable object on the computer graphic display without causing the displayable object to be rotated.
0. 44. An input device for manipulating translational movements of a displayable object on a computer graphic display, comprising:
hand-held housing means adapted for manual movement in free space;
sensing means in the housing means for detecting gravitational orientation; and
inertial means mounted with respect to said housing means and responsive to rotation of the housing means about an axis relative to gravitational orientation for producing a signal indicative of said rotation for manipulating translational movements of the displayable object on the computer graphic display without causing the displayable object to be rotated.
9. A graphical input device for providing a signal to effect the translational movement of a cursor on an interactive computer graphic display comprising:
a housing adapted for manual movement in free space;
an inertial gyroscopic element disposed to spin about one spin axis;
a gimbal supporting the gyroscopic element with respect to the housing; and
a sensor disposed with respect to the gimbal and the housing for producing a signal, in response to rotation of the housing relative to one spin axis, to effect translational movement of the cursor in substantially a single direction for each direction in which the housing is rotated.
14. A graphical An input device for providing a signal to manipulate translational movements of a displayed displayable object on an a computer graphic display, comprising:
a hand-held housing adapted for manual movement in free space; and
an inertial gyroscopic element mounted with respect to said housing, for providing a signal, in response and responsive to rotation of the housing about an axis, to manipulate for producing a signal substantially proportional to said rotation for manipulating translational movements of the displayed displayable object on an interactive the computer graphic display in substantially continuous proportionality to the signal without causing the displayed displayable object to be rotated.
4. A method for providing a signal to effect effecting translational movements of a displayed displayable object on an interactive a computer graphic display using an inertial input device that is manually movable in free space, the method comprising: the steps of:
detecting, by inertial means, rotational movement of the input device about one axis; and
providing producing a first signal responsive substantially proportional to the rotation of the input device about the one axis for effecting translational movements of the displayed displayable object on the computer graphic display in substantially continuous proportionality to the first signal and in a single direction for each direction in which the input device is rotated.
6. A graphical An input device for providing a signal to effect translational movements of a displayed displayable object on an interactive a computer graphic display, comprising:
a hand-held housing adapted for manual movement in free space; and
an inertial gyroscopic element mounted with respect to said housing, for providing a signal, in response and responsive to rotation of the housing about an axis, to effect for producing a signal substantially proportional to said rotation for effecting translational movements of the displayed displayable object on an interactive the computer graphic display in substantially continuous proportionality to the signal and in a single direction for each direction in which the device housing is rotated.
0. 24. An input device for producing a signal to effect translational movements of a displayable object on a computer graphic display, comprising:
a hand-held housing adapted for manual movement in free space;
sensing apparatus in the housing to detect gravitational orientation; and
an inertial gyroscopic element mounted with respect to said housing and responsive to rotation of the housing about an axis relative to the gravitational orientation to produce a signal indicative of said rotation for effecting translational movements of the displayable object on the computer graphic display in substantially a single direction for each direction in which the housing is rotated.
0. 22. A method for effecting translational movements of a displayable object on a computer graphic display using an inertial input device that is manually movable in free space, the method comprising:
sensing gravitational orientation;
detecting rotational movement of the input device about one axis relative to the gravitational orientation; and
producing a first signal substantially proportional to the rotation of the input device about the one axis for effecting translational movements of the displayable object on the computer graphic display in substantially continuous proportionality to the first signal and in a single direction for each direction in which the input device is rotated.
13. A method for controlling translational movements of a displayed displayable object on an interactive a computer graphic display having vertical and horizontal Cartesian coordinate axes in response to one of pitch and yaw rotations of an input device, the method comprising: the steps of:
detecting the pitch or yaw rotation of the input device;
sensing an inertial response to provide produce a signal indicative of substantially proportional to at least one of the pitch and yaw rotations of the input device; and
in response to detecting pitch or yaw movement of the input device, the signal, moving the displayed displayable object a substantially continuously proportional distance in a plane defined by the vertical and horizontal axes on the computer graphic display without rotating the displayed displayable object.
0. 33. An input device for producing a signal to manipulate translational movements of a displayable object on a computer graphic display, comprising:
a hand-held housing adapted for manual movement in free space;
an inertial element mounted with respect to the said housing and responsive to rotation of the housing with respect to an inertial axis of the inertial element for producing a signal indicative of said rotation for manipulating translational movements of the displayable object on the computer graphic display; and
a switch mounted on the housing for manual actuation to one operating state for selectively inhibiting producing said signal, and for actuation to another operating state for enabling producing said signal in response to said rotation.
0. 17. A method for effecting movements of a displayable object on a graphic display having vertical and horizontal Cartesian coordinate axes in response to one of pitch and yaw rotations of an input device, the method comprising:
sensing gravitational orientation;
sensing an inertial response to pitch or yaw rotation of the input device relative to the gravitational orientation to produce a signal indicative of at least one of the pitch and yaw rotations of the input device relative to the gravitational orientation; and
moving the displayable object a distance in a plane defined by the vertical and horizontal axes on the computer graphic display translationally along one of the vertical and horizontal axes in substantially a single direction for each direction in which the input device is rotated.
1. A method for moving effecting movements of a displayed displayable object on an interactive a computer graphic display having vertical and horizontal Cartesian coordinate axes in response to one of pitch and yaw rotations of an input device, the method comprising: the steps of:
detecting the pitch or yaw rotation of the device;
sensing an inertial response to provide pitch or yaw rotation of the input device to produce a signal indicative of proportional to the at least one of the pitch and yaw rotations of the input device; and
in response to the signal indicating the detected pitch or yaw movement of the input device, moving the displayed displayable object a distance in a plane defined by the vertical and horizontal axes on the computer graphic display, the displayed object being moved in substantially continuous proportionality to the signal and translationally along one of the vertical and horizontal axes in substantially a single direction for each direction in which the input device is rotated.
0. 19. A method for effecting movements of a displayable object on a graphic display having vertical and horizontal Cartesian coordinate axes in response to one of pitch and yaw rotations of an input device including an inertial element, the method comprising:
sensing gravitational orientation;
sensing an inertial response to pitch or yaw rotation of the inertial element relative to the gravitational orientation to produce a signal indicative of at least one of the pitch and yaw rotations of the device relative to the gravitational orientation; and
moving the displayable object a distance in a plane defined by the vertical and horizontal axes on the computer graphic display translationally along one of the vertical and horizontal axes in substantially a single direction for each direction in which the input device is rotated.
15. A method for providing producing a signal to control translational movements of a displayed displayable object on an interactive a computer graphic display using an input device including an inertial gyroscopic element that is manually movable in free space, the method comprising: the steps of:
supporting the inertial gyroscopic element with respect to the input device;
actuating the gyroscopic element to exhibit inertia relative to an inertial axis;
detecting rotational movement of the input device relative to the inertial axis of the gyroscopic element; and
providing producing a signal responsive substantially proportional to the rotation of the input device relative to the inertial axis for controlling translational movements of the displayed displayable object in substantially continuous proportionality to the signal without causing the displayed displayable object to be rotated.
3. A method for providing a signal to effect effecting translational movements of a displayed displayable object on an interactive a computer graphic display using an input device including an inertial gyroscopic element that is manually movable in free space, the method comprising: the steps of:
supporting the inertial gyroscopic element with respect to the input device;
actuating the gyroscopic element to exhibit inertia relative to an inertial axis;
detecting rotational movement of the input device relative to the inertial axis of the gyroscopic element; and
providing producing a signal responsive substantially proportional to the rotation of the input device relative to the inertial axis for effecting translational movements of the displayed displayable object on the computer graphic display in substantially continuous proportionality to the signal and in a single direction for each direction in which the input device is rotated.
0. 21. A method for effecting translational movements of a displayable object on a computer graphic display using an input device including an inertial gyroscopic element that is manually movable in free space, the method comprising:
supporting the inertial gyroscopic element with respect to the input device; actuating the gyroscopic element to exhibit inertia relative to an inertial axis;
sensing gravitational orientation;
detecting rotational movement of the input device about the inertial axis of the gyroscopic element relative to the gravitational orientation; and
producing a signal responsive to the rotation of the input device about the inertial axis relative to the gravitational orientation for effecting translational movements of the displayable object on the computer graphic display in substantially a single direction for each direction in which the input device is rotated.
0. 30. A method for producing a signal to control translational movements of a displayable object on a computer display using an input device including an inertial element that is manually movable in free space, the method comprising:
supporting the inertial element with respect to the input device;
sensing gravitational orientation of the input device in free space;
sensing inertia of the input device relative to the sensed gravitational orientation;
detecting rotational movement of the input device with respect to an inertial axis of the inertial element relative to the gravitational orientation; and
producing a signal substantially proportional to the rotation of the input device about the inertial axis relative to the gravitational orientation for controlling translational movements of the displayable object in response to the signal without causing the displayable object to be rotated.
0. 27. An input device for producing a signal to effect translational movement of a displayable object on a graphic display, the input device comprising:
a hand-held housing adapted for manual movement in free space;
an inertial gyroscopic element disposed to spin about one spin axis;
a gimbal supporting the gyroscopic element with respect to the housing and including a center of mass eccentric the spin axis;
a first sensor disposed with respect to the gimbal and the housing and responsive to rotation of the housing relative to one spin axis for producing a signal substantially proportional to said rotation for effecting translational movement of the displayable object in substantially continuous proportionality to the signal and in a single direction for each direction in which the housing is rotated; and
a second sensor in communication with the gimbal for producing an output indicative of gravitational orientation, independent of the orientation of the housing in free space.
2. A The method for effecting translational movements of a displayed object on an interactive computer graphic display as in according to claim 1 further comprising: the steps of:
selectively inhibiting the input device from producing a signal to permit reorientation of the input device without substantially proportional translational movement of the displayed object on the computer graphic display; and
selectively enabling the input device for producing the signal in response to said one of pitch and yaw rotations of the input device.
5. A The method according to claim 4 for providing signals to effect effecting the translational movements on an interactive the computer graphic display along at least one of first and second coordinate axes, using the inertial input device, the method further comprising: the steps of:
detecting, by inertial means, rotational movement of the input device about a second axis not parallel to the one axis;
providing producing a second signal responsive substantially proportional to the rotation of the input device about the second axis; and for effecting translational movements on the display of the displayable object along a first coordinate axis of the computer graphic display in response substantially continuous proportionality to the first signal and in a single direction for each direction in which the input device is rotated about the one axis, or along a second coordinate axis of the computer graphic display in response substantially continuous proportionality to the second signal and in a single direction for each direction in which the input device is rotated about the second axis.
7. A graphical The input device for providing a signal to effect translational movements of a displayed object on an interactive computer graphic display as in according to claim 6, wherein the gyroscopic element comprises an angular position gyroscope.
8. A graphical The input device for providing a signal to effect translational movement of a displayed object on an interactive computer graphic display as in according to claim 7, wherein the angular position gyroscope comprises:
an inertial gyroscopic element disposed to spin about a spin axis;
a gimbal supporting the gyroscopic element with respect to the housing; and
a sensor disposed with respect to the gimbal and the housing for producing said signal in response to rotation of the housing relative to the spin axis.
10. A graphical input device for providing a signal to effect the translational movement of a cursor on an interactive computer graphic display as in claim 9 further comprising a manually operable switch mounted with respect to the housing and operatively connected for selecting inhibiting the graphical input device from producing a signal to permit reorientation of the graphical input device without translational movement of the cursor in response to said signal, and for selectively enabling the graphical input device for producing said signal in response to rotational movement of the housing relative to the spin axis of the gyroscopic element.
11. A graphical input device for providing signals to effect translational movement of a cursor on an interactive computer graphic display as in claim 10 wherein the signal is produced in response to one of pitch and yaw rotational movement of the housing for effecting the translational movement of the cursor along one of vertical and horizontal Cartesian coordinate axes of the display in response to the signal.
12. An interactive computer graphic display system comprising a graphical input device as in claim 11 and further comprising a circuit coupled to the display for effecting the translational movement of the cursor along one of the horizontal and vertical Cartesian coordinate axes of the display in response to the signal.
0. 16. An interactive computer graphic display system comprising an input device according to claim 6 and further comprising a circuit coupled to the computer graphic display for effecting the translational movement of a displayable object along one of horizontal and vertical Cartesian coordinate axes of the computer graphic display in substantially continuous proportionality to the signal.
0. 18. The method according to claim 17, further comprising:
selectively inhibiting the input device from producing the signal to permit reorientation of the input device without translational movement of the displayed object on the computer graphic display; and
selectively enabling the input device for producing the signal in response to said one of pitch or yaw rotations of the input device relative to the gravitational orientation.
0. 20. The method according to claim 19, further comprising:
selectively inhibiting the inertial element from producing the signal to permit reorientation of the input device without translational movement of the displayed object on the computer graphic display; and
selectively enabling the inertial element for producing the signal in response to said one of pitch or yaw rotations of the input device relative to the gravitational orientation.
0. 23. The method according to claim 22 for effecting the translational movements on the computer graphic display along at least one of first and second coordinate axes using the inertial input device, the method further comprising:
detecting rotational movement of the input device about a second axis not parallel to the one axis and relative to the gravitational orientation;
producing a second signal responsive to the rotation of the input device about the second axis for effecting translational movements of the displayable object along a first coordinate axis of the computer graphic display in substantially continuous proportionality to the first signal and in a single direction for each direction in which the input device is rotated about the one axis, or along a second coordinate axis of the computer graphic display in response to the second signal and in a single direction for each direction in which the input device is rotated about the second axis.
0. 25. An input device according to claim 24, wherein the sensing apparatus detects substantially vertical gravitational orientation independent of the orientation of the housing in free space.
0. 26. The input device according to claim 25, wherein the sensing apparatus comprises:
an inertial gyroscopic element disposed to spin about a spin axis;
a gimbal supporting the gyroscopic element with respect to the housing and including a center of mass eccentric the spin axis; and
a sensor communicating with the gimbal for producing an output indicative of the gravitational orientation.
0. 28. An interactive computer graphic display system comprising an input device as in claim 24 and further comprising a circuit coupled to the display for effecting translational movement of the displayable object along one of horizontal and vertical Cartesian coordinate axes of the computer graphic display in response to the rotation of the housing relative to the gravitational orientation.
0. 31. The method according to claim 5 further comprising:
selectively inhibiting producing at least one of the first and second signals to permit reorientation of the device without translational movement of the displayable object on the computer display; and
selectively enabling producing the at least one of the first and second signals in response to rotational movement of the input device about the corresponding one and second axes.
0. 32. The input device according to claim 6 comprising:
a switch mounted on the housing for manual activation to one operating state for selectively inhibiting producing said signal, and for actuation to another operating state for enabling producing said signal in response to said rotation of the housing.
0. 34. The method according to claim 23 further comprising:
selectively inhibiting producing at least one of the first and second signals to permit reorientation of the input device without translational movement of the displayable object on the computer graphic display; and
selectively enabling producing at least the one of the first and second signals in response to said rotation of the input device about the corresponding one and second axes.
0. 35. The input device according to claim 24 comprising:
a switch mounted on said housing for manual actuation to one operating state for selectively inhibiting producing said signal, and for actuation to another operating state for enabling producing said signal in response to said rotation of the housing.
0. 36. The input device according to claim 29 comprising:
a switch mounted on said housing for manual actuation to one operating state for selectively inhibiting producing said signal and for actuation to another operating state for enabling producing said signal in response to said rotation of the housing.
0. 37. The method according to claim 30, further comprising:
selectively inhibiting producing said signal to permit reorientation of the input device without translational movement of the displayable object on the computer graphic display; and
selectively enabling producing said signal in response to said rotation of the input device.
0. 39. The input device according to claim 38 wherein the inertial gyroscopic means comprises an angular position gyroscope.
0. 40. The input device according to claim 38 further comprising:
switch means mounted with respect to the inertial gyroscopic means for selectively inhibiting producing said signal to permit reorientation of the input device without translational movement of the displayable object in response to said signal and for selectively enabling the input device to produce said signal.
0. 41. An interactive computer graphic display system comprising an input device as in claim 38 and further comprising circuit means for effecting translational movement of the displayable object along one of horizontal and vertical Cartesian coordinate axes of the computer graphic display in substantially continuous proportionality to the signal.
0. 42. An input device according to claim 38 comprising:
sensing means for detecting gravitational orientation; and
said inertial gyroscopic means produces said signal indicative of said rotation relative to the gravitational orientation.
0. 43. An interactive computer graphic display system comprising an input device as in claim 42 and further comprising circuit means for effecting translational movement of the displayable object along one of horizontal and vertical Cartesian coordinate axes of the computer graphic display in response to the rotation of the housing relative to the gravitational orientation.
0. 45. The input device according to claim 38 comprising:
switch means with the inertial gyroscopic means for manual activation to one operating state for selectively inhibiting producing said signal, and for actuation to another operating state for enabling producing said signal in response to said rotation of the housing.
0. 46. The input device according to claim 42 comprising:
switch means mounted with said sensing means and said inertial gyroscopic means for manual actuation to one operating state for selectively inhibiting producing said signal, and for actuation to another operating state for enabling producing said signal in response to said rotation.
0. 47. The input device according to claim 44 comprising:
switch means on said housing means for manual actuation to one operating state for selectively inhibiting producing said signal, and for actuation to another operating state for enabling producing said signal in response to said rotation of said housing means.

This is a continuation of application Ser. No. 08/406,727, filed on Mar. 20, 1995, now abandoned, which is a continuation of Ser. No. 08/000,651, filed on Jan. 5, 1993, now U.S. Pat. No. 5,440,326, which is a continuation of Ser. No. 07/497,127, filed on Mar. 21, 1990, now abandoned.

1. Field

The present invention relates to the field of hand-held computer controllers. More specifically, the present invention relates to a hand-held gyroscopic pointer adapted for use as a cursor-control device for a computer.

2. Art Background

A. Computer controllers:

Historically, computer instructions have taken the form of commands entered as words on a keyboard. More recently, pointing devices and icon-based interface techniques have been developed which permit a computer user to select tasks and to enter commands by moving a cursor on a computer display screen in response to movement of a pointing device. Pointing devices used for this task have included joysticks, trackballs and mouse controllers. One early use of a mouse as a pointing device for an icon-based computer interlace was at Xerox PARC. More recently, the mouse has become well known as a computer input device with its use on the Apple Macintosh line of computers and on the workstation computers distributed by Sun Microsystem.

However, a mouse, requires a relatively large and flat 2-dimensional surface on which to move. Typically, this surface must be unobstructed and dedicated to mouse movement and measure over 9″×9″ interlace interface box 185 to outer housing 175 and returns data signals from shaft angle encoder sensing optics 165. In the preferred embodiment interface box 185 translates signals from the optical sensing system 165 into serial data for an RS-232 port. Wall adapter 190 provides D.C. power for motor 105 and shalt shaft angle encoder sensing optics 165.

The construction details of the inner and outer gimbals is are shown in further detail in FIG. 2. FIG. 2 is an expanded perspective view of inner gimbal 115 and bearing 122. Inner gimbal 115 includes a circular plug 205 which fits within the inner race of bearing 122. A conductive pin 210, having a diameter smaller than that of plug 205, is mounted concentrically with plug 205 and electrically coupled to motor 205. Pin 210 is preferably made of a low-friction conductive material such as carbon-teflon and designed to protrude from the inner race of bearing 122. The diameter of pin 210 is smaller than the diameter of the inner race so as not to contact the inner race and to minimize the friction of the rotating contact. A stainless steel spring 215 is mounted to gimbal frame 135 and aligned with and in electrical contact with protruding surface 220 of pin 210.

Spring 215 is electrically coupled to a D.C. power source through outer gimbal 140. Spring 215 presses against pin 210 providing a low friction electrical connection between gimbal frame 135 and inner module 110. Inner gimbal 120 and outer gimbals 140 and 145 are constructed in an identical manner.

Inner module 110 has a hemispherical outer surface with an optical pattern which interacts with shaft angle encoder sensing optics 165 to sense the rotation of inner module 110 around the axis of rotation through gimbals 115 and 120. This optical pattern is illustrated in FIG. 3. The optical pattern on inner module 110 is constructed by first painting the hemispherical surface with a highly reflective aluminum flaked paint and then machining grooves of 0.015 inch depth and width along “lines of longitude” from gimbal 115 towards gimbal 120 along the surface. The grooves are machined to within 30 degrees of each inner gimbal and are 0.015 inches apart at 30 degrees from each gimbal. The pattern causes the spacing between the groove centerlines to widen to approximately 0.04 inches at the middle (“equator”) of inner module 110. Inner module 110 is molded from a non-reflective black plastic. Thus the grooved portions of inner module 110. where the reflective paint has been machined off, are non-reflective. This provides a precise optical pattern on inner module 110 having a relatively high contrast ratio.

And A second optical pattern is machined into gimbal frame 135 along a cylindrical section 170 of gimbal frame 135. This pattern interacts with shalt shaft angle encoder sensing optics 165 for sensing rotation of gimbal frame 135 around its axis of rotation through gimbals 140 and 145. This cylindrical section is geometrically centered about the axis of rotation of gimbal frame 135, which passes through gimbals 140 and 145. As with the optical pattern on the inner module 110, the optical pattern on gimbal frame 135 is constructed by applying reflective paint to cylindrical section 170 and then machining grooves of 0.015 inch depth and width on the surface of the cylinder.

These grooves are machined along lines parallel to the axis of rotation of gimbal frame 135 and evenly spaced so that the light and dark strips are of equal width. Cylindrical section 170 is displaced slightly from the center of gimbal frame 135 so as not lo interfere with the interaction of shaft angle encoder sensing optics 165 and the optical pattern on inner module 110. Specifically, the closest edge of cylindrical section 170 is spaced approximately 0.15 inches away from the “equator” of frame 170 passing through inner gimbals 115 and 120.

Shaft angle encoder sensing optics 165 interact with the optical pattern on inner module 110 so as to determine the rotation of the inner module 110 about its axis of rotation. More specifically, shaft angle encoder sensing optic 165 include sources for illuminating the patterns, lenses for focusing images of the patterns, and photodetectors for detect a detecting dark or light areas. Referring to FIG. 3, a first LED 305 is mounted to shock frame 160 at an angle of 30 degrees from vertical in a plane parallel to the axis through gimbals 140 and 145 so as to floodlight an area 310 of the optical pattern on inner module 110. This area is centered on the “equator” of frame 135 so as to provide maximum range of detectable movement in both directions. Lens 315 and mirror 320 focus and reflect the image of the illuminated optical pattern onto quad photodiode 325. Lens 315 is an injection molded lens of approximately ⅛ inch in diameter having a focal length of approximately 0.2 inches.

Quad photodiode 325 comprises four photodiodes, 402, 404, 406 and 408, located in a row as illustrated in FIG. 4. The sides of quad photodiode 325 are aligned with the edges of the projected image of the optical pattern on inner module 110. One period of the projected image of the optical pattern on inner module 110 (one light and one dark bar) nominally covers the quad photodiode 325, which comprise four photodiodes centered 0.02 inches apart. Photodiodes 402 and 406 are counted coupled to comparator 420 410. Photodiodes 404 and 408 are coupled to comparator 410 420. The output V1 of comparator 410 is thus in phase quadrature with the output V2 of comparator 420. These outputs are then detected by conventional means to determine the rotation of the inner module. An example of phase quadrature resolution is provided in U.S. Pat. No. 4,346,989 titled Surveying Instrument, issued to Alfred F. Gori Gort and Charles E. Moore Aug. 31, 1982 and assigned to the Hewlett-Packard Company. A prototype of this embodiment of the present invention results in a resolution of approximately 100 counts per inch.

Shaft angle encoder sensing optics 165 also interacts with the optical pattern on gimbal frame 160 so as to determine the rotation of gimbal frame 135 about its axis of rotation. More specfically, a second sensing system, similar to the one described but oriented 90 degrees with respect to the first, is positioned on frame 160 so as to interact with the optical pattern on frame 135 and to detect rotation of frame 135 about its axis of rotation. Referring again to FIG. 3, a second LED 330 is mounted to shock frame 160 at an angle of 30 degrees from vertical in a plane parallel to the axis through gimbals 115 and 120 in alignment with cylindrical section 170 so as to floodlight an area 335 of the optical pattern on cylindrical section 170. Lens 340 and mirror 320 focus and reflect the image of the illuminated optical pattern onto quad photodiode 345. Lens 340 is an injection molded lens of approximately ⅛ inch in diameter having a focal length of approximately 0.2 inches.

Quad photodiode 345 comprises four photodiodes located in a row and is identical in construction to quad photodiode 325 illustrated in FIG. 4. The sides of quad photodiode 345 are aligned with the edges of the projected image of the optical pattern on gimbal frame 135. FIG. 5 is an illustration of the preferred embodiment of a gyroscopic pointing device 500 coupled to a computer 502 and computer display 505. Computer 502 is adapted so that changing the pitch of controller 500 relative to the gravity vector charges changes the vertical position of cursor 510 on computer display 505. That is, rotating the controller forward (“pitch”) causes the cursor to drop on a vertical computer screen, rotating it back causes the cursor to drop on a vertical computer screen,rotating it back causes the cursor to rise, as if the controller was pointing at the cursor. Similarly, rotating the controller from side to side (“roll”) changes the horizontal position of cursor 510 on computer display 505. That is, rotating the controller left causes the cursor to move left on a vertical computer screen, rotating it right causes the cursor to move to the right, again, as it if the controller was pointing at the cursor. Controller 500 further includes a thumb operated push button 520 and has a rounded hemispherically shaped bottom portion 525 adapted for smoothly rocking on a flat surface when the pitch and roll of controller 500 is varied while resting on a flat surface. This can be a two position switch, where initial pressure on the switch activates the controller and causes the cursor to move in response to the controller, and a second position of the switch results in a “pick” or “select” signal being transmitted to the computer.

FIG. 6 is a top view of an alternative embodiment of the present invention. FIG. 7 is a top perspective view of the same embodiment. Specifically, FIGS. 6 and 7 illustrate a controller shaped so as to be hand held in a manner such that the palm will be facing down while controller 610 is resting on a flat surface. The under side of controller 610 is rounded to facilitate changes of its orientation with respect to vertical. A palm button 620 is actuated when the controller is grasped, thus permitting the controller to be deactivated, moved or reoriented, then reactivated. A pick button 630 is located for selective activation by a users lingers user's fingers in a manner similar to the use of a pick button on a mouse controller.

The embodiment of FIGS. 6 and 7 includes a first gyroscope as discussed with regards to FIGS. 1-4 for the measurement of pitch and roll. Further, it includes a second gyroscope, as illustrated in FIG. 8, for measurement of yaw about the vertical axis. Specifically, a rotating gyroscopic element 810 is mounted in a two-degree-of freedom gimbal system with its spin axis 820 in a horizontal direction. In the preferred embodiment a mass gives the gyroscope a pendulosity at right angles to spin axis 820. More specifically, gyroscope 810 is mounted to inner frame 815. Inner frame 815 is mounted to gimbal frame 825 by inner gimbals 845. Gimbal frame 825 is mounted to an outer housing 860 by gimbal 850. A shaft angle encoder 870 is coupled to detect the rotation of gimbal frame 825 relative to outer housing 860. Oscillations are damped out by applying an antipendulous torque caused by liquid flow of a viscous fluid through a constriction in a tube, as in damper 840. Computer 502 is further adapted to convert the angle measured by shaft angle encoder 870. This conversion could be to rotation of the cursor or a cursor-selected object or for providing a “z” input for a three dimensional display or a two-dimensional display simulating a three dimensional view.

While the invention has been particularly taught and described with reference to the preferred embodiment, those versed in the art rill will appreciate that minor modifications in form and detail may be made without departing from the spirit and scope of the invention. For instance, although the illustrated embodiment teaches one system of shaft angle encoders, many alternative systems could be used for detecting the orientation of the gyroscopic controller. Further, while the preferred embodiment leaches teaches a vertically oriented gyroscope and detection of two angles from vertical such as in an artificial horizon instrument. Other gyroscopic orientations, such as those used for directional gyroscopes, could be substituted. Further, while the present invention teaches the detection of two angles from a vertically oriented gyroscope and one angle from a horizontally oriented gyroscope, two angles could be detected from the horizontal gyroscope, and one from the vertical gyroscope. Further, many techniques equivalent techniques to the pendulous technique are known for orienting gyroscopes. Accordingly, all such modifications are embodied within the scope of this patent as and properly come within our my contribution to the art and as are particularly pointed out by the following claims.

Quinn, Thomas J.

Patent Priority Assignee Title
Patent Priority Assignee Title
2309853,
3782205,
4267731, Feb 11 1980 Honeywell INC Force balanced vibratory rate sensor
4489609, Dec 08 1981 British Technology Group Limited Gyroscopes
4580006, Jun 14 1984 Method and apparatus for providing two dimensional positioning data signals
4601206, Sep 16 1983 Ferranti International PLC Accelerometer system
4639547, Oct 05 1984 Kontron Elektronik GmbH Marking device for use with inductive measuring sensor
4644793, Sep 07 1984 MARCONI COMPANY LIMITED, THE, THE GROVE, WARREN LANE, STANMORE, MIDDLESEX, HA7 4L7 ENGLAND, A BRITISH COMPANY Vibrational gyroscope
4831544, Nov 21 1986 Tokyo Keiki Co., Ltd. Attitude and heading reference detecting apparatus
4839838, Mar 30 1987 IDHL HOLDINGS, INC Spatial input apparatus
4862152, Jan 25 1985 Sonic positioning device
5068645, Oct 14 1987 3M Innovative Properties Company Computer input device using an orientation sensor
5097707, Jan 18 1989 GEC-Marconi Limited Rotation sensor
5142655, Oct 14 1987 3M Innovative Properties Company Computer input device using an orientation sensor
5287119, Oct 14 1987 3M Innovative Properties Company Computer input device using an orientation sensor
5288078, Oct 14 1988 David G., Capper Control interface apparatus
5329276, Dec 19 1990 Kabushiki Kaisha Yaskawa Denki Multidimensional signal input device
5363120, Oct 14 1987 3M Innovative Properties Company Computer input device using orientation sensor
5453758, Jul 31 1992 Sony Corporation Input apparatus
JP62143124,
/////////////////////////////////
Executed onAssignorAssigneeConveyanceFrameReelDoc
Oct 12 2000Thomson Licensing(assignment on the face of the patent)
Dec 02 2003GYRATION, INC YOSHIDA, LARRY MINORU SECURITY INTEREST SEE DOCUMENT FOR DETAILS 0141920970 pdf
Dec 02 2003GYRATION, INC TARPLEY, DAVIDSECURITY INTEREST SEE DOCUMENT FOR DETAILS 0141920970 pdf
Dec 02 2003GYRATION, INC VONDERSCHMITT, BERNARD V & THERESA S SECURITY INTEREST SEE DOCUMENT FOR DETAILS 0141920970 pdf
Dec 02 2003GYRATION, INC QUINN, THOMAS J SECURITY INTEREST SEE DOCUMENT FOR DETAILS 0141920970 pdf
Dec 02 2003GYRATION, INC New York Life Insurance CompanySECURITY INTEREST SEE DOCUMENT FOR DETAILS 0141920970 pdf
Dec 02 2003GYRATION, INC Berg & Berg Enterprises, LLCSECURITY INTEREST SEE DOCUMENT FOR DETAILS 0141920970 pdf
Dec 02 2003GYRATION, INC HUNTINGTON VENTURE PARTNERS, LLCSECURITY INTEREST SEE DOCUMENT FOR DETAILS 0141920970 pdf
Dec 02 2003GYRATION, INC HUNTINGTON TECHNOLOGY, FUND, LPSECURITY INTEREST SEE DOCUMENT FOR DETAILS 0141920970 pdf
Dec 02 2003GYRATION, INC EXCELSIOR VENTURE PARTNERS III, LLCSECURITY INTEREST SEE DOCUMENT FOR DETAILS 0141920970 pdf
Jan 22 2004GYRATION, INC MAEZAWA, YOSHIHIROSECURITY AGREEMENT0143010103 pdf
Jan 22 2004GYRATION, INC HAWTHORNE, GREGORY & SUSANSECURITY AGREEMENT0143010103 pdf
Jan 22 2004GYRATION, INC RICHARD E BLOCK & JANE C BLOCK, TEE BLOCK FAMILY TRUST DTD 5 29 1992SECURITY AGREEMENT0143010103 pdf
Jan 22 2004GYRATION, INC BLOCK, CHARLES A SECURITY AGREEMENT0143010103 pdf
Jan 22 2004GYRATION, INC BLOCK, CATHERINE S SECURITY AGREEMENT0143010103 pdf
Jan 22 2004GYRATION, INC ATSUSHI ASADASECURITY AGREEMENT0143010103 pdf
Aug 16 2004HUNTINGTON VENTURE PARTNERS, LLCGYRATION, INC RELEASE OF SECURITY INTEREST0151160380 pdf
Aug 16 2004MAEZAWA, YOSHIHIROGYRATION, INC RELEASE OF SECURITY INTEREST0151160380 pdf
Aug 16 2004New York Life Insurance CompanyGYRATION, INC RELEASE OF SECURITY INTEREST0151160380 pdf
Aug 16 2004QUINN, THOMAS J GYRATION, INC RELEASE OF SECURITY INTEREST0151160380 pdf
Aug 16 2004TARPLEY, DAVIDGYRATION, INC RELEASE OF SECURITY INTEREST0151160380 pdf
Aug 16 2004VONDERSCHMITT, BERNARD V , JOINT DECL OF TRUST DTD 1 04 96GYRATION, INC RELEASE OF SECURITY INTEREST0151160380 pdf
Aug 16 2004VONDERSCHMITT, THERESA S , JOINT DECL OF TRUST DTD 1 04 96GYRATION, INC RELEASE OF SECURITY INTEREST0151160380 pdf
Aug 16 2004HUNTINGTON TECHNOLOGY FUND, LPGYRATION, INC RELEASE OF SECURITY INTEREST0151160380 pdf
Aug 16 2004GREGORY & SUSAN HAWTHORNEGYRATION, INC RELEASE OF SECURITY INTEREST0151160380 pdf
Aug 16 2004EXCELSIOR VENTURE PARTNERS III, LLCGYRATION, INC RELEASE OF SECURITY INTEREST0151160380 pdf
Aug 16 2004BLOCK, JANE C , TEE BLOCK FAMILY TRUST DTD 5 29 1992GYRATION, INC RELEASE OF SECURITY INTEREST0151160380 pdf
Aug 16 2004BLOCK, RICHARD E , TEE BLOCK FAMILY TRUST DTD 5 29 1992GYRATION, INC RELEASE OF SECURITY INTEREST0151160380 pdf
Aug 16 2004BLOCK, CHARLES A GYRATION, INC RELEASE OF SECURITY INTEREST0151160380 pdf
Aug 16 2004BLOCK, CATHERINE S GYRATION, INC RELEASE OF SECURITY INTEREST0151160380 pdf
Aug 16 2004Berg & Berg Enterprises, LLCGYRATION, INC RELEASE OF SECURITY INTEREST0151160380 pdf
Aug 16 2004ASADA, ATSUSHIGYRATION, INC RELEASE OF SECURITY INTEREST0151160380 pdf
Aug 16 2004YOSHIDA, LARRY MINORU GYRATION, INC RELEASE OF SECURITY INTEREST0151160380 pdf
Date Maintenance Fee Events
Sep 10 2010M1553: Payment of Maintenance Fee, 12th Year, Large Entity.
Sep 30 2010STOL: Pat Hldr no Longer Claims Small Ent Stat
Oct 01 2010R2553: Refund - Payment of Maintenance Fee, 12th Yr, Small Entity.


Date Maintenance Schedule
Aug 17 20134 years fee payment window open
Feb 17 20146 months grace period start (w surcharge)
Aug 17 2014patent expiry (for year 4)
Aug 17 20162 years to revive unintentionally abandoned end. (for year 4)
Aug 17 20178 years fee payment window open
Feb 17 20186 months grace period start (w surcharge)
Aug 17 2018patent expiry (for year 8)
Aug 17 20202 years to revive unintentionally abandoned end. (for year 8)
Aug 17 202112 years fee payment window open
Feb 17 20226 months grace period start (w surcharge)
Aug 17 2022patent expiry (for year 12)
Aug 17 20242 years to revive unintentionally abandoned end. (for year 12)