Integrated guidance and control method for high-speed morphing wing aircraft

被引：0
|
作者：
He, Hao [1 ]
Wang, Peng [1 ]
机构：
[1] College of Aerospace Science and Engineering, National University of Defense Technology, Changsha,410073, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2024年 / 45卷
关键词：
D O I：
10.7527/S1000-6893.2024.30692
中图分类号：
学科分类号：
摘要：
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