Mathematical Model of a Monocopter Based on Unsteady Blade-Element Momentum Theory-Reference-Cited by-同舟云学术

Mathematical Model of a Monocopter Based on Unsteady Blade-Element Momentum Theory

Published:2015-11 Issue:6 Volume:52 Page:1905-1913
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Matič Gašper¹,Topič Marko¹,Jankovec Marko¹

Affiliation:

1. Department of Electronics, University of Ljubljana, SI-1000 Ljubljana, Slovenia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C033098

Reference23 articles.

1. HoughtonJ.HoburgW. “Fly-by-Wire Control of a Monocopter,” Massachusetts Inst. of Technology TR-16.622, Cambridge, MA, 2008, pp. 1–36, https://docs.google.com/file/d/0B3suSD5Oh7F8SU9qcEtMamhCY0k/edit [retrieved 17 June 2014].

2. Pitch and Heave Control of Robotic Samara Micro Air Vehicles

3. Spincopter Wing Design and Flight Control

4. A Multi-Scale Simulation Methodology for the Samarai Monocopter ?UAV

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