Flight Dynamics Modeling and Dynamic Stability Analysis of Tilt-Rotor Aircraft
The tilt-rotor aircraft has often been proposed as a means to increase the maximum speed of the conventional helicopter. The tilt-rotor aircraft consists of three primary flight modes that are the helicopter flight mode in low forward speed flight, airplane flight mode in high forward speed flight,...
| Published in: | International Journal of Aerospace Engineering |
|---|---|
| Main Authors: | , , , |
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2019-01-01
|
| Online Access: | http://dx.doi.org/10.1155/2019/5737212 |