The Simulation and Analysis of the Tilt Rotor Aircraft Model Transition
- 10.2991/mcei-16.2016.46How to use a DOI?
- Simulation; XV-15; Tilt rotor
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.
- © 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
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 -