Modeling and Simulation of Control Actuation System with Fuzzy-PID Logic Controlled Brushless Motor Drives for Missiles Glider Applications

A control actuation system has been used extensively in automotive, aerospace, and defense applications. The major challenges in modeling control actuation system are rise time, maximum peak to peak overshoot, and response to nonlinear system with percentage error. This paper addresses the challenge...

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Detalles Bibliográficos
Autores principales: Muniraj, Murali, Arulmozhiyal, Ramaswamy
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Hindawi Publishing Corporation 2015
Materias:
Research Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4647030/
https://www.ncbi.nlm.nih.gov/pubmed/26613102
http://dx.doi.org/10.1155/2015/723298

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4647030/
https://www.ncbi.nlm.nih.gov/pubmed/26613102
http://dx.doi.org/10.1155/2015/723298

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