Design of Guidance Laws with Falling Angle Constraint and Coupling of Seeker Dynamics

Aiming at the problems of the dynamic coupling between the guided rocket projectile body and the seeker, a guidance law design method with falling angle constraint is proposed. Firstly, considering the coupling effect between the seeker and the projectile body during flight, the two-degree-of-freedo...

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Bibliographic Details
Main Author: Lu Jiaojiao, Dong Meng, Guo Zhengyu
Format: Article
Language:zho
Published: Editorial Office of Aero Weaponry 2023-02-01
Series:Hangkong bingqi
Subjects:
Online Access:https://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/2022-00110.pdf