Development of A Fixed-Wing mini UAV with Transitioning Flight Capability-Reference-Cited by-同舟云学术

Development of A Fixed-Wing mini UAV with Transitioning Flight Capability

Published:2017-06-02 Issue: Volume: Page:
ISSN:
Container-title:35th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Bronz Murat¹,Smeur Ewoud J.²,Garcia de Marina Hector¹,Hattenberger Gautier¹

Affiliation:

1. French Civil Aviation University

2. Delft University of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3739

Reference17 articles.

1. Using a multispectral autonomous unmanned aerial remote sensing platform (AggieAir) for riparian and wetlands applications

2. Development of a Long Endurance Mini-UAV: ETERNITY

3. Design of A High-Performance Tailless MAV Through Planform Optimization

4. 4Lustosa, L., Defay, F., and Moschetta, J.M. “Development of the flight model of a tilt-body MAV,” 2014International Micro Air Vehicle Conference and Competition (IMAV 2014), Delft, NL, 2014, pp.157-163, Thanks to IMAV 2014. The originalPDFis available at TU Delft Library Open Access repository: http://repository.tudelft.nl/conferencepapers/.

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