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.

Patent No.:

US 8195345 B1

PDF
Full Text
Expired
Date of Patent:
Jun. 05, 2012

Filed:

Aug. 05, 2010
Applicants:

Hanafy M. Omar, Dhahran, SA;

Mohammad A. Abido, Dhahran, SA;

Inventors:

Hanafy M. Omar, Dhahran, SA;

Mohammad A. Abido, Dhahran, SA;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01C 23/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

The method for generating an integrated guidance law for aerodynamic missiles uses a strength Pareto evolutionary algorithm (SPEA)-based approach for generating an integrated fuzzy guidance law, which includes three separate fuzzy controllers. Each of these fuzzy controllers is activated in a unique region of missile interception. The distribution of membership functions and the associated rules are obtained by solving a nonlinear constrained multi-objective optimization problem in which final time, energy consumption, and miss distance are treated as competing objectives. A Tabu search is utilized to build a library of initial feasible solutions for the multi-objective optimization algorithm. Additionally, a hierarchical clustering technique is utilized to provide the decision maker with a representative and manageable Pareto-optimal set without destroying the characteristics of the trade-off front. A fuzzy-based system is employed to extract the best compromise solution over the trade-off curve.


Find Patent Forward Citations

Omar, Hanafy. (2012). Method of generating an integrated fuzzy-based guidance law for aerodynamic missiles (U.S. Patent No. 8195345). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/8195345

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