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,...

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Bibliographic Details
Main Authors: Ke Lu, Chunsheng Liu, Chunhua Li, Renliang Chen
Format: Article
Language:English
Published: Wiley 2019-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2019/5737212
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