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

Hierarchical tracker and method

Patent 5341143 Issued on August 23, 1994. Estimated Expiration Date: Icon_subject August 23, 2011. 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

3076961

3108270

3501762

3724783

3737120

3740002

Arithmatic circuit for bang-bang seekers
Patent #: 3970269
Issued on: 07/20/1976
Inventor: Conforti

Prestored area correlation tracker
Patent #: 4106726
Issued on: 08/15/1978
Inventor: Emmons ,   et al.

Correlation system for multiple-sensor reconnaissance vehicle
Patent #: 4122521
Issued on: 10/24/1978
Inventor: Rick ,   et al.

Target sensing and homing system
Patent #: 4160974
Issued on: 07/10/1979
Inventor: Stavis

More ...

Inventors

Application

No. 234710 filed on 08/19/1988

US Classes:

342/64, With map matching244/3.15, Automatic guidance244/3.16, Optical (includes infrared)244/3.17, Optical correlation342/52, COMBINED WITH DIVERSE TYPE RADIANT ENERGY SYSTEM342/55, With television342/62Missile or spacecraft guidance

Examiners

Primary: Gregory, Bernarr E.

Attorney, Agent or Firm

International Classes

G01S 013/66
G06F 015/50

Abstract

Method and apparatus for guiding a projectile to a target in a scene using a scene imaging sensor in which the projectile has a guidance and control system for aiming the projectile. A first tracker analyzes the scene and selects a first track point representative of a target and a first confidence value serving as a reliability measure of the first selected track point. A second tracker analyzes the scene and selects a second track point representing the target and a second confidence value which serves as a reliability measure of the second selected track point. Each of said trackers are constructed and arranged to operate independently in a manner that is substantially statistically uncorrelated with respect to each other. A joint confidence value based on track point proximity, convergence and divergence is generated from the tracker data and a composite confidence index is calculated from the first and second confidence values and the joint confidence value. The first and second track points are linearly combined pursuant to one of a set of rules selected by the confidence index to provide a new track point which is outputted to the projectile guidance and control system and new start track points are generated that are specially suited to restart the trackers in a new operation cycle.

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