U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Spatial input apparatus

Patent 4839838 Issued on June 13, 1989. Estimated Expiration Date: Icon_subject March 30, 2007. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

2996268

3597598

3729129

Acceleration error compensated attitude sensing and control apparatus and method
Patent #: 4038876
Issued on: 08/02/1977
Inventor: Morris

Calculator interface
Patent #: 4151596
Issued on: 04/24/1979
Inventor: Howells

Optical strapdown inertia system
Patent #: 4315693
Issued on: 02/16/1982
Inventor: Walker

Three-axis accelerometer having flexure bearing with overload protection
Patent #: 4398417
Issued on: 08/16/1983
Inventor: Shutt

Self-extinguishing polyolefin compositions
Patent #: 4420577
Issued on: 12/13/1983
Inventor: Bertelli ,   et al.

Apparatus and method for measuring specific force and angular rate
Patent #: 4445376
Issued on: 05/01/1984
Inventor: Merhav

Point location and graphics display apparatus
Patent #: 4506336
Issued on: 03/19/1985
Inventor: Hird

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Inventors

Application

No. 07/032305 filed on 03/30/1987

US Classes:

708/141, Including specific nonkeyboard-type information entry345/157Cursor mark position control device

Examiners

Primary: Harkcom, Gary V.
Assistant: Shaw, Dale M.

Attorney, Agent or Firm

International Classes

G06F 3/033 (20060101)
G01P 15/18 (20060101)
G01P 15/08 (20060101)

Abstract

A three-dimensional spatial input apparatus including a series of coplanar, single axis accelerometers configured to provide information on translation along and rotation around a set of orthogonal axes. A preprocessing computer determines the acceleration values output by the accelerometers and converts these values into a series of acceleration, velocity and position values in relation to the axis system, with corrections based on a change in the influence of gravity on the device as it rotates. The values are transmitted to an object control computer which takes appropriate action, including moving a cursor, rotating a displayed object, and controlling remote devices. The spatial input apparatus can have an attached pointer and be used as a three-dimensional digitizer in conjunction with the object control computer.

Other References

  • W Neuman & R. Sproull, Principles of Interactive Computer Graphics, pp. 147-157 (1979)
  • Interactive Computer Graphics Systems, Petrocelli Books Inc., p. 169 (1982)
  • McDonnell Douglas, 3 SPACE product literature
  • Sundstrand Data Control, Inc. QA-700 & QA-2000 Servo Accelerometer product and application literature
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