The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Mar. 06, 2012

Filed:

Oct. 08, 2007
Applicants:

Thu-van Luu, Lumberton, NJ (US);

Jeffrey B. Boka, Lumberton, NJ (US);

Purusottam Mookerjee, Bridgewater, NJ (US);

Michael J. Harcourt, Sicklerville, NJ (US);

Inventors:

Thu-Van Luu, Lumberton, NJ (US);

Jeffrey B. Boka, Lumberton, NJ (US);

Purusottam Mookerjee, Bridgewater, NJ (US);

Michael J. Harcourt, Sicklerville, NJ (US);

Assignee:

Lockheed Martin Corporation, Bethesda, MD (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01S 13/66 (2006.01); G01S 13/88 (2006.01); F42B 15/01 (2006.01); G01S 13/00 (2006.01); F42B 15/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

A method and a system for sensing a boosting target missile, estimate position and velocity and boost acceleration parameters of the target missile, and control an interceptor missile to the target missile. A boost-phase missile target state estimator estimates at least acceleration, velocity, and position using an acceleration template for the target vehicle. The nominal template is incorporated into an extended Kalman filter which corrects the nominal template acceleration with the filter states to predict future thrust acceleration, velocity and position. The correction can compensate for motor burn variations and missile energy management (lofted/depressed trajectory).


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