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:
Oct. 16, 2012

Filed:

Nov. 06, 2007
Applicants:

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

Purusottam Mookerjee, Bridgewater, NJ (US);

Naresh R. Patel, Bellmawr, NJ (US);

Inventors:

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

Purusottam Mookerjee, Bridgewater, NJ (US);

Naresh R. Patel, Bellmawr, NJ (US);

Assignee:

Lockheed Martin Corporation, Bethesda, MD (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F41G 7/30 (2006.01); F42B 15/01 (2006.01); F41G 7/00 (2006.01); F42B 15/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

A method for engaging a target missile includes sensing the position of the target and of an interceptor missile, and determining time-to-go to intercept and direction of thrust of the interceptor. A one-step intercept solution is determined based on position estimates of the target and the interceptor and is used to iteratively estimate at least two components of a three-dimensional unit thrust vector, and apply updated guidance commands to the interceptor. A system for thrust vector control of an interceptor against a target missile includes a processor for receiving sensed target signals, determining a one-step initial solution to produce time-to-go and current direction of thrust of the interceptor, iteratively estimating at least two components of a three-dimensional unit thrust vector, and producing a guidance vector for application to the interceptor.


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