Nonlinear Dynamic Inversion Based Attitude Control for a hovering quad tiltrotor eVTOL vehicle
Author:
Affiliation:
1. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0134
Reference33 articles.
1. Adaptive Control of a Quadcopter in the Presence of large/complete Parameter Uncertainties
2. Design of Flight Control System for a Small Unmanned Tilt Rotor Aircraft
3. Modeling and Incremental Nonlinear Dynamic Inversion Control of a Novel Unmanned Tiltrotor
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