Dynamic Modeling and Active Morphing Trajectory-Attitude Separation Control Approach for Gull-Wing Aircraft

Morphings are usually used for aircrafts to achieve a better performance in variable environment, whereas this paper focuses on how to achieve a trajectory-attitude separation control effect with an active morphing strategy. Aimed at this target, a systemic work, including modeling, linearization, a...

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Bibliographic Details
Main Authors: Tianhao Guo, Zhongxi Hou, Bingjie Zhu
Format: Article
Language:English
Published: IEEE 2017-01-01
Series:IEEE Access
Subjects:
Online Access:https://ieeexplore.ieee.org/document/8014442/