Nonlinear Control of a Fixed-Wing UAV using Support Vector Machine
Author:
Affiliation:
1. California Polytechnic State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0107
Reference18 articles.
1. Nonlinear Control Systems
2. A dynamic inversion based control law with application to the high angle-of-attack research vehicle
3. Dynamic Inversion Based Control Concept with Application to an Unmanned Aerial Vehicle
4. Stability and flying qualities robustness of a dynamic inversion aircraft control law
5. Gain-scheduled missile autopilot design using linear parameter varying transformations
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