Principle and Realization Method of Serpentine Maneuver at the Ballistic End of Aircraft

The end of the aircraft is facing increasingly severe air defense threat, so it is necessary to maneuver the end to improve the probability of the penetration of the aircraft. This paper expounds the guidance problem of the snake maneuver of the vehicle, and deeply analyzes the maneuver and guidance...

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Published inIEEE ... Information Technology and Mechatronics Engineering Conference (ITOEC ... ) (Online) Vol. 8; pp. 1554 - 1560
Main Authors Zhu, Haokun, Li, Fanbiao, Yu, Xiaojun, Cao, ChenYu, Liu, Chuang
Format Conference Proceeding
LanguageEnglish
Published IEEE 14.03.2025
Subjects
Aircraft
Atmospheric modeling
End of Ballistic
Guidance Law
Information technology
Maneuvering Penetration
Mathematical models
Mechatronics
Oscillators
Serpentine Maneuvering
Stability analysis
Target tracking
Trajectory
Vectors
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ISSN2693-289X
DOI10.1109/ITOEC63606.2025.10968837

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Summary:The end of the aircraft is facing increasingly severe air defense threat, so it is necessary to maneuver the end to improve the probability of the penetration of the aircraft. This paper expounds the guidance problem of the snake maneuver of the vehicle, and deeply analyzes the maneuver and guidance principles of three snake-like maneuver methods based on overload vector cycle change, velocity vector cycle change and displacement vector cycle change. And this paper put forward the corresponding implementation method. The feasibility of the three principles and the implementation method is verified through the mathematical simulation; Finally, the comparative analysis summarizes the advantages and disadvantages of the above three methods.
ISSN:2693-289X
DOI:10.1109/ITOEC63606.2025.10968837