Compound Cooperative Guidance for High Parabolic Trajectory in Three-Dimensional Space
Cooperative guidance problem of multiple missile system in three-dimensional space is investigated in this paper. Guidance commands in pitch plane and lateral plane of initial guidance, mid-course guidance and terminal guidance are designed, and the rules of shift guidance in different guidance stag...
Guardado en:
Autor principal: | Zhao Qilun,Song Xun,Wang Xiaodong,Wang Mengyi |
---|---|
Formato: | article |
Lenguaje: | ZH |
Publicado: |
Editorial Office of Aero Weaponry
2021
|
Materias: | |
Acceso en línea: | https://doaj.org/article/08adb432e4724d62b074de30dd5fce54 |
Etiquetas: |
Agregar Etiqueta
Sin Etiquetas, Sea el primero en etiquetar este registro!
|
Ejemplares similares
-
Effectiveness Evaluation Technology of Missile Cooperative Guidance Considering Missile Miss Distance and Formation Structure
por: Guo Zhengyu,Li Yaomin,Wang Chaolei,Shi Rongzong
Publicado: (2021) -
Three Dimensional Impact Time Control Guidance Law with Field of View Constraint
por: Ruan Cong,Wen Qiuqiu,Zhang Wenjie
Publicado: (2021) -
An Anti-Wing Flexure Velocity+Attitude Matching Rapid Transfer Alignment Algorithm
por: Cheng Haibin,Lu Hao,Wang Jinda
Publicado: (2021) -
Study on the Influence of Disturbance Rejection Rate on the Performance of Roll-Pitch Semi-Strapdown Guidance System
por: Hu Yifan, Ren Hongguang, Yang Shuo, Zhang Yuekun
Publicado: (2021) -
A Scheme of Ground Velocity Measurement Assisted by Missile-Borne Radar
por: Zhao Yihuan, Yin Jianyong, Yang Hongqiao, Chen Wei, Liao Huashan
Publicado: (2021)