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