Transitional Flight Control of Tail-Sitter Vertical Takeoff and Landing Mini Unmanned Aerial Vehicle-Reference-Cited by-同舟云学术

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Transitional Flight Control of Tail-Sitter Vertical Takeoff and Landing Mini Unmanned Aerial Vehicle

Published:2007-05-07 Issue: Volume: Page:
ISSN:
Container-title:AIAA Infotech@Aerospace 2007 Conference and Exhibit
language:
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Author:

Kubo Daisuke¹,Suzuki Shinji¹

Affiliation:

1. The University of Tokyo

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-2752

Reference14 articles.

1. 1Unmanned aircraft systems roadmap 2005-2030. United States Department of Defense, electronic document (http://www.acq.osd.mil/usd/Roadmap%20Final2.pdf), August2005.

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1. Multimode Controller design and flight test for Tailsitter UAV without elevon;2023 6th International Conference on Electronics Technology (ICET);2023-05-12

2. Transition control of a tail-sitter UAV using recurrent neural networks;2020 International Conference on Unmanned Aircraft Systems (ICUAS);2020-09

3. Transitional Control Architecture and Methodology for a Twin Rotor Tailsitter;Journal of Guidance, Control, and Dynamics;2014-07

4. Indoor Experimentation and Flight Test Results for a Twin Rotor Tailsitter Unmanned Air Vehicle;AIAA Guidance, Navigation, and Control (GNC) Conference;2013-08-15

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