Linear Extended State Observer-Based Motion Synchronization Control for Hybrid Actuation System of More Electric Aircraft

Moving towards the more electric aircraft (MEA), a hybrid actuator configuration provides an opportunity to introduce electromechanical actuator (EMA) into primary flight control. In the hybrid actuation system (HAS), an electro-hydraulic servo actuator (EHSA) and an EMA operate on the same control...

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Detalles Bibliográficos
Autores principales: Wang, Xingjian, Liao, Rui, Shi, Cun, Wang, Shaoping
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2017
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5712900/
https://www.ncbi.nlm.nih.gov/pubmed/29068392
http://dx.doi.org/10.3390/s17112444

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5712900/
https://www.ncbi.nlm.nih.gov/pubmed/29068392
http://dx.doi.org/10.3390/s17112444

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