Parametric Design and Optimization of Multi-Rotor Aerial Vehicles-Reference-Cited by-同舟云学术

Parametric Design and Optimization of Multi-Rotor Aerial Vehicles

Published:2014 Issue: Volume: Page:1-25
ISSN:1931-6828
Container-title:Applications of Mathematics and Informatics in Science and Engineering
language:
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Author:

Ampatis C.,Papadopoulos E.

Publisher

Springer International Publishing

Link

http://link.springer.com/content/pdf/10.1007/978-3-319-04720-1_1

Reference12 articles.

1. F. Kendoul, Survey of advances in guidance, navigation, and control of unmanned rotorcraft systems, Journal of Field Robotics, Vol. 29, No 2, pp. 315–378, March/April 2012,

2. Q. Jiang, et al, Analysis and Synthesis of Mult-Rotor Aerial Vehicles, Proceedings of the ASME 2011 International Design Engineering Technical Conferences & Computers and Information in Engineering Conference, IDETC/CIE 2011, August 28–31, Washington, DC, USA, DETC2011-47114, 2011.

3. D. Langkamp, et al, An engineering development of a novel hexrotor vehicle for 3D applications, Proceedings Micro Air Vehicles Conference 2011, Summer edition, 2011.

4. N. Fernandes, Design and construction of a multi-rotor with various degrees of freedom, M.S. Thesis, Technical Univ. of Lisboa, 2011.

5. F. Bohorquez, et al., Design, Analysis and Hover Performance of a Rotary Wing Micro Air Vehicle, Journal of the American Helicopter Society, Vol. 48, No 2, pp. 80–90, 2003.

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