Design of Multi-Missile Cooperative Guidance Law Based on Pulse Engine Characteristics

Design of Multi-Missile Cooperative Guidance Law Based on Pulse Engine Characteristics

Aiming at the design problem of multi-missile cooperative guidance law for attacking high-speed targets, a design method of multi-missile cooperative guidance law based on the working characteristics of pulse engine is proposed. Firstly, the relative motion equation of missile and target is solved....

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Bibliographic Details
Main Author: Pan Hui, Zhang Zhenlin, Guo Chao
Format: Article
Language:zho
Published: Editorial Office of Aero Weaponry 2022-02-01
Series:Hangkong bingqi
Subjects:
|cooperative guidance|consistency theory|angle constraint|impulse engine characteristics|sliding mode variable structure control|discrete guidance|missile
Online Access:https://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/2021-00069.pdf

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https://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/2021-00069.pdf

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