Incremental Model Predictive Attitude Control for Morphing Aircraft: A Weak Model-Dependent Control Method

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Date
2026
Author
Cai, Guangbin
Zheng, Hui
Wang, Yongchao
Zhang, Shiyuan
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Abstract
AbstractIn this article, an incremental model predictive attitude control for morphing aircraft with variable wingspans and sweepback angles is proposed. This method does not require a concrete mathematical model of the system, thus reducing the ...
URI
http://yetl.yabesh.ir/yetl1/handle/yetl/4314121
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