Flight Dynamics Modeling and Control of a Novel Catapult Launched Tandem-Wing Micro Aerial Vehicle With Variable Sweep

Flight Dynamics Modeling and Control of a Novel Catapult Launched Tandem-Wing Micro Aerial Vehicle With Variable Sweep

In this paper, the variable sweep is used as a replacement for the conventional control surfaces for flight control on a tandem-wing micro aerial vehicle (MAV). This configuration allows the MAV to be folded into and launched from a tubular catapult while also retaining an adequately high effectiven...

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Bibliographic Details
Main Authors: Liang Gao, Hongzhe Jin, Jie Zhao, Hegao Cai, Yanhe Zhu
Format: Article
Language:English
Published: IEEE 2018-01-01
Series:IEEE Access
Subjects:
Tandem-wing
variable sweep
catapult launch
dynamic coupling
morphing aircraft
Kane method
Online Access:https://ieeexplore.ieee.org/document/8417416/

Internet

https://ieeexplore.ieee.org/document/8417416/

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