摘要
A cooperative encirclement interception method based on virtual aiming points is proposed for intercepting the high-speed maneuvering targets in near-space in three-dimensional scenarios. A calculation method for the ideal interception time of interceptor groups is derived by analyzing the maneuvering envelope of target and considering the guidance characteristics of the interceptors. Thus,the problem of intercepting the high-speed maneuvering targets is transformed into a problem of hitting a specific point on a fixed spatial plane at a predetermined time and angle. Based on the ideal interception time and angle of attack,the virtual aiming points are selected in space to guide the interceptors,ensuring that the impact angles meet the head-on interception conditions,thereby reducing the requirement for the speed of interceptor. The interception tests are conducted on two typical C-type and S-type maneuvering targets through numerical simulation. The results demonstrate that the proposed method is used to successfully intercept C-type and S-type maneuvering targets with different maneuvering intensities, achieve a minimum group miss distance of less than 3 meters,and enable the impact angle meet the requirements of head-on interception angle.
| 投稿的翻译标题 | A Cooperative Encirclement Interception Method for High-speed Maneuvering Target in Head-on Engagement |
|---|---|
| 源语言 | 繁体中文 |
| 期刊论文编号 | 240979 |
| 期刊 | Binggong Xuebao/Acta Armamentarii |
| 卷 | 46 |
| 期 | 9 |
| DOI | |
| 出版状态 | 已出版 - 30 9月 2025 |
| 已对外发布 | 是 |
关键词
- cooperative encirclement interception
- head on interception
- maneuvering target
- near space target
- virtual aiming point
学术指纹
探究 '针对高速机动目标的逆轨协同围捕方法' 的科研主题。它们共同构成独一无二的学术指纹。引用此
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver