Design, Construction, and Testing of a Folding-Wing, Tube-Launched Micro Air Vehicle-Reference-Cited by-同舟云学术

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Design, Construction, and Testing of a Folding-Wing, Tube-Launched Micro Air Vehicle

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Henry Jonathon¹,Schwartz David¹,Soukup Michael²,Altman Aaron²

Affiliation:

1. Air Force Research Laboratory

2. University of Dayton

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1451

Reference4 articles.

1. 2Brian Roth, C. Peters and William A. Crossley, "Aircraft Sizing with Morphing as an Independent Variable", AIAA 2002-5840.

Cited by 5 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. Design and Flight Test of a Tube-Launched Unmanned Aerial Vehicle;Aerospace;2024-02-03

2. Design and Analysis of a Deployment Mechanism with Clearance Compensation for High Stiffness Missile Wings;Drones;2022-08-17

3. Flight dynamics modeling and stability analysis of a tube-launched tandem wing aerial vehicle during the deploying process;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-04-27

4. Design, Construction, and Flight Testing of the World's Fastest Micro-Scale Quadcopter;55th AIAA Aerospace Sciences Meeting;2017-01-05

5. On Fixed-Wing Micro-Air Vehicles with Hovering Capabilities;46th AIAA Aerospace Sciences Meeting and Exhibit;2008-01-07

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