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...
Main Authors: | , , |
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Format: | Article |
Language: | English |
Published: |
IEEE
2017-01-01
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Series: | IEEE Access |
Subjects: | |
Online Access: | https://ieeexplore.ieee.org/document/8014442/ |