Modeling, Control, and Flight Testing of a Small Ducted Fan Aircraft-Reference-Cited by-同舟云学术

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Modeling, Control, and Flight Testing of a Small Ducted Fan Aircraft

Published:2005-06-19 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference and Exhibit
language:
Short-container-title:

Author:

Johnson Eric¹,Turbe Michael¹

Affiliation:

1. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-6281

Reference15 articles.

1. GoldenEye: The Clandestine UAV

2. 3Johnson, E. N. "Limited Authority Adaptive Flight Control," Ph.D. Thesis,Georgia Institute of Technology, 2000, pp.15-16,42.

3. Adaptive Trajectory Control for Autonomous Helicopters

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1. Modelling and numerical analysis of attitude control flaps of a UAV;International Journal on Interactive Design and Manufacturing (IJIDeM);2023-07-24

2. Control Effectiveness Enhancement for the Hovering/Cruising Transition Control of a Ducted Fan UAV;Journal of Intelligent & Robotic Systems;2022-08

3. Modeling and Hovering Attitude Control of a Prototype Tandem Ducted Fan Vehicle;Journal of Intelligent & Robotic Systems;2014-10-14

4. Modeling and Hovering Control of an Ducted-Fan UAV in Low Speed Crosswind;Advanced Materials Research;2012-02

5. Performance, Flight Testing of a Shrouded Rotor Micro Air Vehicle in Edgewise Gusts;Journal of Aircraft;2012-01

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