Design and Control of a Stable Invertible Coaxial Actuated ROtorcraft (SICARO)
Author:
Affiliation:
1. Engineering Product Development (EPD) Pillar of Singapore University of Technology and Design (SUTD),Singapore,487372
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10196083/10196094/10196142.pdf?arnumber=10196142
Reference14 articles.
1. Achieving Efficient Controlled Flight with A Single Actuator
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4. Observing the angle of attack of the tip-path plane from rotor blade measurements;trainelli,2015
5. Mathematical Model of a Monocopter Based on Unsteady Blade-Element Momentum Theory
Cited by 1 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. Harnessing the Differential Flatness of Monocopter Dynamics for the Purpose of Trajectory Tracking in a Stable Invertible Coaxial Actuated ROtorcraft (SICARO);2024 IEEE International Conference on Robotics and Automation (ICRA);2024-05-13
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