Cyclic Blade Pitch Control Without a Swashplate for Small Helicopters

Author:

Paulos James1,Yim Mark1

Affiliation:

1. University of Pennsylvania, Philadelphia, Pennsylvania 19104

Funder

Division of Computing and Communication Foundations

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Cited by 13 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Bio-inspired classification and evolution of multirotor Micro Aerial Vehicles (MAVs): A comprehensive review;Robotics and Autonomous Systems;2024-09

2. Characterization of different hinge angles for swashplateless micro aerial robots;Engineering Science and Technology, an International Journal;2024-07

3. Spring-Damped Underactuated Swashplateless Rotor on a Bicopter Unmanned Aerial Vehicle;Machines;2024-04-28

4. Swashplateless-Elevon Actuation for a Dual-Rotor Tail-Sitter VTOL UAV;2023 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS);2023-10-01

5. HALO: A Safe, Coaxial, and Dual-Ducted UAV Without Servo;2023 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS);2023-10-01

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