A Simple Attitude Control of Quadrotor Helicopter Based on Ziegler-Nichols Rules for Tuning PD Parameters

An attitude control strategy based on Ziegler-Nichols rules for tuning PD (proportional-derivative) parameters of quadrotor helicopters is presented to solve the problem that quadrotor tends to be instable. This problem is caused by the narrow definition domain of attitude angles of quadrotor helico...

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Detalles Bibliográficos
Autores principales: He, ZeFang, Zhao, Long
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Hindawi Publishing Corporation 2014
Materias:
Research Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4295143/
https://www.ncbi.nlm.nih.gov/pubmed/25614879
http://dx.doi.org/10.1155/2014/280180

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4295143/
https://www.ncbi.nlm.nih.gov/pubmed/25614879
http://dx.doi.org/10.1155/2014/280180

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