Integrated Missile Guidance and Control Design with Angle of Attack Constraint

This paper proposes a composite guidance method with angle of attack constraint for the integrated guidance and control system with the problems of target maneuver, missile parameter perturbation and missile angle of attack constraint. Firstly, an integrated guidance and control system is establishe...

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Bibliographic Details
Main Author: Wu Di, Wang Xinming, He Jingang, Zhang Jinpeng, Li Shihua
Format: Article
Language:zho
Published: Editorial Office of Aero Weaponry 2022-06-01
Series:Hangkong bingqi
Subjects:
Online Access:https://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/2021-00229.pdf