Global Singularity-Free Aerodynamic Model for Algorithmic Flight Control of Tail Sitters

Author:

Lustosa Leandro R.1,Defaÿ François1,Moschetta Jean-Marc1

Affiliation:

1. ISAE-SUPAERO, University of Toulouse, 31400 Toulouse, France

Funder

Conselho Nacional de Desenvolvimento Científico e Tecnológico

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Cited by 19 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. Differential Flatness of Lifting-Wing Quadcopters Subject to Drag and Lift for Accurate Tracking;IEEE Transactions on Industrial Electronics;2024-10

2. Dynamic Feedback Linearization of Flying Wings With Real-time Newton-Raphson Iterations;2024 European Control Conference (ECC);2024-06-25

3. Modelling and Hovering Stabilisation of a Free-Rotating Wing UAV;2024 International Conference on Unmanned Aircraft Systems (ICUAS);2024-06-04

4. Flight Validation of a Global Singularity-Free Aerodynamic Model for Flight Control of Tail Sitters;2024 IEEE International Conference on Robotics and Automation (ICRA);2024-05-13

5. Vector ducted propeller aerodynamic modeling and verification testing;Journal of Physics: Conference Series;2024-03-01

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