A Hybrid Control with PID–Improved Sliding Mode for Flat-Top of Missile Electromechanical Actuator Systems

Electromechanical actuator (EMA) systems are widely employed in missiles. Due to the influence of the nonlinearities, there is a flat-top of about 64 ms when tracking the small-angle sinusoidal signals, which significantly reduces the performance of the EMA system and even causes the missile traject...

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Detalles Bibliográficos
Autores principales: Zhou, Man, Mao, Dapeng, Zhang, Mingyue, Guo, Lihong, Gong, Mingde
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2018
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6308980/
https://www.ncbi.nlm.nih.gov/pubmed/30558334
http://dx.doi.org/10.3390/s18124449

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6308980/
https://www.ncbi.nlm.nih.gov/pubmed/30558334
http://dx.doi.org/10.3390/s18124449

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