Scalability of Cyclic Control without Blade Pitch Actuators
Author:
Affiliation:
1. University of Pennsylvania, Philadelphia
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0532
Reference15 articles.
1. An underactuated propeller for attitude control in micro air vehicles
2. Flight performance of a swashplateless micro air vehicle
3. Cyclic Blade Pitch Control for Small UAV Without a Swashplate
4. AprilTag: A robust and flexible visual fiducial system
5. Hunt, G. K. “Similarity Requirements for Aeroelastic Models of Helicopter Rotors,” Tech. Rep. RAE 72005 (ARC 33730), 1972.
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