Velocity-Aided Attitude Estimation for Helicopter Aircraft Using Microelectromechanical System Inertial-Measurement Units

This paper presents an algorithm for velocity-aided attitude estimation for helicopter aircraft using a microelectromechanical system inertial-measurement unit. In general, high- performance gyroscopes are used for estimating the attitude of a helicopter, but this type of sensor is very expensive. W...

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Detalles Bibliográficos
Autores principales: Lee, Sang Cheol, Hong, Sung Kyung
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2016
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5191082/
https://www.ncbi.nlm.nih.gov/pubmed/27973429
http://dx.doi.org/10.3390/s16122102

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5191082/
https://www.ncbi.nlm.nih.gov/pubmed/27973429
http://dx.doi.org/10.3390/s16122102

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