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

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
https://doi.org/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.
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Proceedings
2016 6th International Conference on Mechatronics, Computer and Education Informationization (MCEI 2016)
Part of series
Advances in Intelligent Systems Research
Publication Date
December 2016
ISBN
978-94-6252-282-4
ISSN
1951-6851
DOI
https://doi.org/10.2991/mcei-16.2016.46How to use a DOI?
Open Access
This is an open access article distributed under the CC BY-NC license.

Cite this article

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  - 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  - https://doi.org/10.2991/mcei-16.2016.46
ID  - Ji2016/12
ER  -