Load Alleviation for a Tilt-Rotor Aircraft in Airplane Mode
Author:
Affiliation:
1. University of Liverpool, Liverpool, L69 3GH, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.13565
Reference12 articles.
1. First Steps in the Development of Handling Qualities Criteria for a Civil Tilt Rotor
2. Load alleviation in tilt rotor aircraft through active control; modelling and control concepts
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