Skip to content

Opening book details…

About this Computer Science article

Robust Attitude Tracking Control Scheme for a Multi-body Spacecraft Using a Radial Basis Function Network and Terminal Sliding Mode by Yuan, Changqing (author);Zhong, Yanhua (author);Zhang, Jingrui (author);Li, Hongbuo (author);Yang, Guojun (author);Shen, Ying (author) is a Computer Science article available to read on EtoBox.

It is typically read by researchers, students, and practitioners in Computer Science.

Author
Yuan, Changqing (author);Zhong, Yanhua (author);Zhang, Jingrui (author);Li, Hongbuo (author);Yang, Guojun (author);Shen, Ying (author)
Publisher
Cambridge University Press
Published
2014
Field
Computer Science (Physical Sciences)

More by Yuan, Changqing (author);Zhong, Yanhua (author);Zhang, Jingrui (author);Li, Hongbuo (author);Yang, Guojun (author);Shen, Ying (author)

Browse all works by Yuan, Changqing (author);Zhong, Yanhua (author);Zhang, Jingrui (author);Li, Hongbuo (author);Yang, Guojun (author);Shen, Ying (author)