Guidance, Navigation, and Control System Design for Tripropeller Vertical-Take-Off-and-Landing Unmanned Air Vehicle
Author:
Affiliation:
1. Ohio University, Athens, Ohio 45701
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.34476
Reference28 articles.
1. Stabilization and nonlinear control for a novel trirotor mini-aircraft
2. Real-Time Control of a Small-Scale Helicopter Having Three Rotors
3. The Stanford testbed of autonomous rotorcraft for multi agent control (STARMAC)
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