Modeling and Incremental Nonlinear Dynamic Inversion Control of a Novel Unmanned Tiltrotor
Author:
Affiliation:
1. Dipartimento di Ingegneria Industriale e dell’Informazione, Second University of Naples, 81031 Aversa, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033183
Reference21 articles.
1. Design of Flight Control System for a Small Unmanned Tilt Rotor Aircraft
2. Modeling and Control of a Small Autonomous Aircraft Having Two Tilting Rotors
3. Evaluation of Longitudinal Desired Dynamics for Dynamic-Inversion Controlled Generic Reentry Vehicles
4. ItoD.GeorgieJ.ValasekJ.WardD. T. “Reentry Vehicle Flight Controls Design Guidelines: Dynamic Inversion,” NASA TP-2002-210771, March 2002.
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