Integrated fuzzy guidance law for high maneuvering targets based on proportional navigation guidance
An integrated fuzzy guidance (IFG) law for a surface to air homing missile is introduced. The introduced approach is a modification of the well-known proportional navigation guidance (PNG) law. The IFG law enables the missile to approach a high maneuvering target while trying to minimize control eff...
Main Authors: | L Hassan, h sadati, j karimi |
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Format: | Article |
Language: | English |
Published: |
Iran University of Science and Technology
2013-12-01
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Series: | Iranian Journal of Electrical and Electronic Engineering |
Subjects: | |
Online Access: | http://ijeee.iust.ac.ir/browse.php?a_code=A-10-958-1&slc_lang=en&sid=1 |
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