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...
Main Author: | |
---|---|
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 |