Wind Tunnel Manoeuvre Rig: A Multi-DOF Test Platform for Model Aircraft
Author:
Affiliation:
1. University of Bristol
2. Nanjing University of Aeronautics and Astronautics
3. De Montfort University
Publisher
American Institute of Aeronautics and Astronautics
Reference7 articles.
1. Wind-Tunnel Investigation of Commercial Transport Aircraft Aerodynamics at Extreme Flight Conditions
2. A Multi-Degree-of-Freedom Rig for the Wind Tunnel Determination of Dynamic Data
3. Mathematical modelling, simulation, and estimation of aircraft parameters using five degree-of-freedom dynamic test rig
4. Multi-Degree-of-Freedom Wind-Tunnel Maneuver Rig for Dynamic Simulation and Aerodynamic Model Identification
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Quaternion-Based Attitude Estimation of an Aircraft Model Using Computer Vision;Sensors;2024-06-12
2. Control for Novel 3-DOF Flight Testing in a Wind Tunnel;2024 UKACC 14th International Conference on Control (CONTROL);2024-04-10
3. Motion Estimation of an Aircraft Model Using Computer Vision;AIAA SCITECH 2024 Forum;2024-01-04
4. Minimally Constrained Flight Simulation in Wind Tunnel;Journal of Aircraft;2019-07
5. Experimental Investigation of Aerodynamic Hysteresis Using a Five-Degree-of-Freedom Wind-Tunnel Maneuver Rig;Journal of Aircraft;2019-05
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