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Nonlinear Model and Ballistic Impact of Body Aerodynamics for Canard Dual-Spin Aircraft

Targeting the nonlinear issues of the canard dual-spin aircraft, which relies on the high-speed rotation of the afterbody for flight stability and achieves trajectory correction by adjusting the roll angle of the low-speed rotating forebody to alter aerodynamics, the establishment of an accurate aer...

Deskribapen osoa

Gorde:
Xehetasun bibliografikoak
Egile Nagusiak: Xinxin Zhao, Jinguang Shi, Huajie Ren, Zhongyuan Wang
Formatua: Artigo
Hizkuntza:Inglês
Argitaratua: MDPI AG 2025-06-01
Saila:Aerospace
Gaiak:
Sarrera elektronikoa:https://www.mdpi.com/2226-4310/12/6/558
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