| 3rd International Symposium on Resource Exploration and Environmental Science | |
| Simulation Research on Dynamic RCS Characteristics of Cruise Missile | |
| 生态环境科学 | |
| Wen, Baoqian^1 ; Wang, Tao^1 ; Cheng, Kun^2 | |
| Rocket Force University of Engineering, Xi'an | |
| 710025, China^1 | |
| Rocket Force Equipment Department, Beijing | |
| 100085, China^2 | |
| 关键词: Attitude angle; Cruise missile; Dynamic RCS; FEKO; Track simulation; | |
| Others : https://iopscience.iop.org/article/10.1088/1755-1315/300/2/022170/pdf DOI : 10.1088/1755-1315/300/2/022170 |
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| 学科分类:环境科学(综合) | |
| 来源: IOP | |
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【 摘 要 】
The target radar cross section (RCS) is an important basis for air defense radar detection and tracking. Aiming at the influence of flight attitude change on the target RCS during the actual flight process, a dynamic RCS method based on the target static RCS database and the target motion track is proposed. The dynamic RCS characteristics of the cruise missile under the actual motion track are simulated, which is convenient for the air defense radar to accurately and quickly detect the target, and further provide operational advice for the best timing of the air defense weapon interception target. The simulation results show that the method can quickly and accurately obtain the dynamic RCS characteristics of the air target. The analysis of the simulation results can provide a theoretical reference for the air defense weapon to intercept the enemy's incoming target.
【 预 览 】
| Files | Size | Format | View |
|---|---|---|---|
| Simulation Research on Dynamic RCS Characteristics of Cruise Missile | 793KB |
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