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An online-implementable differential evolution tuned all-aspect guidance law

Raghunathan, T and Ghose, Debasish (2010) An online-implementable differential evolution tuned all-aspect guidance law. In: Control Engineering Practice, 18 (10). pp. 1197-1210.

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Official URL: http://dx.doi.org/10.1016/j.conengprac.2010.05.013


This paper proposes a differential evolution based method of improving the performance of conventional guidance laws at high heading errors, without resorting to techniques from optimal control theory, which are complicated and suffer from several limitations. The basic guidance law is augmented with a term that is a polynomial function of the heading error. The values of the coefficients of the polynomial are found by applying the differential evolution algorithm. The results are compared with the basic guidance law, and the all-aspect proportional navigation laws in the literature. A scheme for online implementation of the proposed law for application in practice is also given. (c) 2010 Elsevier Ltd. All rights reserved.

Item Type: Journal Article
Publication: Control Engineering Practice
Publisher: Elsevier Science
Additional Information: Copyright of this article belongs to Elsevier Science.
Keywords: Missile guidance; Optimal control; Genetic algorithm; Online control; Real-time
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering(Formerly Aeronautical Engineering)
Date Deposited: 11 Nov 2010 10:23
Last Modified: 11 Nov 2010 10:23
URI: http://eprints.iisc.ac.in/id/eprint/33567

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