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

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The Simulation and Analysis of the Tilt Rotor Aircraft Model Transition

Authors
Min Ji, Ning Wang, Chong Zhao
Corresponding Author
Min Ji
Available Online December 2016.
DOI
10.2991/mcei-16.2016.46How to use a DOI?
Keywords
Simulation; XV-15; Tilt rotor
Abstract

Based on the results of simulation, operating characteristics of XV-15 tilt rotor aircraft were qualitative analyzed, and when to fade out the rotor control was determined, and also the conversion corridor was determined. Inside the conversion corridor, a conversion route that had the least trimmed pitch attitude was suggested.

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-16.2016.46
ISSN
1951-6851
DOI
10.2991/mcei-16.2016.46How 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  - Min Ji
AU  - Ning Wang
AU  - Chong Zhao
PY  - 2016/12
DA  - 2016/12
TI  - The Simulation and Analysis of the Tilt Rotor Aircraft Model Transition
BT  - Proceedings of the 2016 6th International Conference on Mechatronics, Computer and Education Informationization (MCEI 2016)
PB  - Atlantis Press
SP  - 218
EP  - 221
SN  - 1951-6851
UR  - https://doi.org/10.2991/mcei-16.2016.46
DO  - 10.2991/mcei-16.2016.46
ID  - Ji2016/12
ER  -