Trimming Analysis Method of Quad Tilt Rotor Based on Aerodynamic Interference Model
Author:
Affiliation:
1. Yangzhou Collaborative Innovation Research Institute, 225000 Yangzhou, People’s Republic of China
2. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China
Funder
Priority Academic Program Development of Jiangsu Higher Education Institutions
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference35 articles.
1. Effects of an Image Plane on the Tiltrotor Fountain Flow
2. Flowfield and Acoustic Measurements from a Model Tiltrotor in Hover
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2. Modeling and Passivity-based Control of a Dual-tilt rotor UAV;2022 41st Chinese Control Conference (CCC);2022-07-25
3. Modeling and control of a class of urban air mobility tiltrotor aircraft;Aerospace Science and Technology;2022-05
4. On Structural Parameter Optimization Method for Quad Tilt-Wing UAV Based on Indirect Size Estimation of Domain of Attraction;IEEE Access;2022
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