Nonlinear Agile Control Test Bed for a Fixed Wing Aircraft in a Constrained Environment

Author:

Sobolic Frantisek1,How Jonathan1

Affiliation:

1. Massachusetts Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Reference13 articles.

1. 1General Atomics Aeronautical Systems, “Predator Unmanned Aerial Vehicle,” Available at http://www.gaasi.com/products/predator.php,2007.

2. Flight Modeling and Experimental Autonomous Hover Control of a Fixed Wing Mini-UAV at High Angle of Attack

3. Aerodynamic aspects of aircraft dynamics at high angles of attack /AGARD Lecture/

4. Experiments in Fixed-Wing UAV Perching

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4. Global Singularity-Free Aerodynamic Model for Algorithmic Flight Control of Tail Sitters;Journal of Guidance, Control, and Dynamics;2019-02

5. Real-Time Flight Simulation of Highly Maneuverable Unmanned Aerial Vehicles;Journal of Aircraft;2014-11

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