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

Method of inferring sensor attitude through multi-feature tracking

Patent 5647015 Issued on July 8, 1997. Estimated Expiration Date: Icon_subject June 7, 2015. 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

Tracking and/or guidance systems
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Issued on: 07/31/1979
Inventor: Voles

Dual mode guidance system
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Issued on: 04/13/1982
Inventor: Hueber

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Patent #: 4746976
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Patent #: 4969036
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Inventor: Bhanu, et al.

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Patent #: 4993662
Issued on: 02/19/1991
Inventor: Barnes, et al.

Guiding an unmanned vehicle by reference to overhead features
Patent #: 5155684
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Inventors

Assignee

Application

No. 487204 filed on 06/07/1995

US Classes:

382/103, Target tracking or detecting382/278, Correlation701/222Using star tracker

Examiners

Primary: Boudreau, Leo H.
Assistant: Kelley, Chris

Attorney, Agent or Firm

International Class

G06K 009/20

Abstract

A method for inferring precise sensor attitude information in a tracking sensor system begins with storing at a first time a reference image in a memory associated with tracking sensor. Next, the method includes sensing at a second time a second image. The sensed image comprises a plurality of sensed feature locations. The method further includes determining the position of the tracking sensor at the second time relative to its position at the first time and then forming a correlation between the sensed feature locations and the predetermined feature locations as a function of the relative position. The method results in an estimation of a tracking sensor pose that is calculated as a function of the correlation. Because the method is primarily computational, implementation requires no new hardware in a tracking sensor system other than that which may be required to provide additional computational capacity.

Other References

  • S. Singh et al, "Nonlinear Decoupling Sliding Mode Control and Attitude Control of Spacecraft." Sep. 1989 pp. 621-63
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