Title: Fuzzy guidance law for surface-to-air missile in the command control systems
Abstract: A fuzzy guidance law for surface-to-air missile in the command control system is proposed. The performance of the designed guidance law is compared with the famous and widely used guidance law, known as proportional navigation guidance law. The simulation results are proved the effectiveness of the novel guidance law.
Publication Year: 2012
Publication Date: 2012-11-01
Language: en
Type: article
Indexed In: ['crossref']
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Cited By Count: 2
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