Proceedings of the 2016 6th International Conference on Mechatronics, Computer and Education Informationization (MCEI 2016)

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Tilt Rotor Aircraft Coupling Research

Authors
Chong Zhao, Ning Wang
Corresponding Author
Chong Zhao
Available Online December 2016.
DOI
10.2991/mcei-16.2016.122How to use a DOI?
Keywords
Nonlinear; Linear mode; Simulation; CouplingNonlinear; Linear mode; Simulation; CouplingNonlinear; Linear mode; Simulation; CouplingNonlinear; Linear mode; Simulation; CouplingNonlinear; Linear mode; Simulation; CouplingNonlinear; Linear mode; Simulation; CouplingNonlinear; Linear mode; Simulation;
Abstract

Through the rotor machine balancing linearization, the nonlinear model of this paper on the basis of the linear model, through the simulation analysis model of dynamic coupling and coupling operation, through the characteristic root configuration method for inner loop decoupling control, realize the dynamic decoupling.

Copyright
© 2017, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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Volume Title
Proceedings of the 2016 6th International Conference on Mechatronics, Computer and Education Informationization (MCEI 2016)
Series
Advances in Intelligent Systems Research
Publication Date
December 2016
ISBN
10.2991/mcei-16.2016.122
ISSN
1951-6851
DOI
10.2991/mcei-16.2016.122How to use a DOI?
Copyright
© 2017, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

Cite this article

risenwbib
TY  - CONF
AU  - Chong Zhao
AU  - Ning Wang
PY  - 2016/12
DA  - 2016/12
TI  - Tilt Rotor Aircraft Coupling Research
BT  - Proceedings of the 2016 6th International Conference on Mechatronics, Computer and Education Informationization (MCEI 2016)
PB  - Atlantis Press
SP  - 586
EP  - 589
SN  - 1951-6851
UR  - https://doi.org/10.2991/mcei-16.2016.122
DO  - 10.2991/mcei-16.2016.122
ID  - Zhao2016/12
ER  -