Record Details


Field	Value

Title	Fuzzy logic implementation of proportional navigation guidance

Creator	RAJASEKHAR, V SREENATHA, AG

Description	Guidance is one of the most important tasks in the success of a missile mission. There are several problems that create inaccuracies in guidance. Fuzzy logic controllers (FLCs) have the ability to perform effectively even in situations where the information about the plant is inexact and the operating conditions are uncertain. A FLC based on the popular Proportional Navigation Guidance (PNG) law is proposed in this work. The FLC alters the value of the equivalent Navigational Constant to reap the maximum benefits in terms of the missile performance. The FLC is introduced into the guidance loop and the results are compared with those obtained with the conventional PNG law. It has been shown that the FLC needs lower peak acceleration and fuel than the conventional PNG law in all the cases under consideration even when noise and flight control system dynamics of the first order are introduced into the loop. (. .

Publisher	PERGAMON-ELSEVIER SCIENCE LTD

Date	2011-08-24T12:00:22Z 2011-12-26T12:56:53Z 2011-12-27T05:46:23Z 2011-08-24T12:00:22Z 2011-12-26T12:56:53Z 2011-12-27T05:46:23Z 2000

Type	Article

Identifier	ACTA ASTRONAUTICA, 46(1), 17-24 0094-5765 http://dx.doi.org/10.1016/S0094-5765(99)00189-7 http://dspace.library.iitb.ac.in/xmlui/handle/10054/10877 http://hdl.handle.net/10054/10877

Language	en

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