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Dynamic modeling and bifurcation analysis of agile turn parafoil-missile system
Hong-Miao ZHOU Jianqiao Yu Yong Yu
Acta Aeronautica et Astronautica Sinica . 0, (): 0 -0 .  DOI: 10.7527/1000-6893.2023.29012

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Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics

All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341