导管式风扇飞行阵列系统的海上应用:反舰导弹诱饵

Junho Jeong, Beomyeol Yu, Taegyun Kim, Seungkeun Kim, J. Suk, H. Oh
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引用次数: 3

摘要

本文提出了一种利用由多个单模块组成的导管式风扇飞行阵列系统作为诱饵的应用。每个单独的模块都有一个传统的管道风扇配置,可以单独飞行。简要介绍了单模块和连接阵列的运动学和动力学模型。在此基础上,采用滑模控制(SMC)和比例-积分-导数(PID)方法构建了一个层次结构的控制系统。同时,对多枚反舰导弹和一艘目标舰进行了简单运动学分析。针对导弹系统,设计了一种比例导航制导律。此外,提出了一种考虑预期信号功率(ESP)的顺序逻辑。ESP通过控制站的导引头和诱饵信号模型计算,然后控制站向多个诱饵发送路径规划命令。在可视化环境下进行了数值模拟,验证了两枚导弹和两个诱饵的诱饵任务。仿真结果表明,分离的单个模块能够有效地实现诱饵的作用。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Maritime application of ducted-fan flight array system: Decoy for anti-ship missile
This paper proposes a decoy application using a ducted-fan flight array system which consists of multiple single modules. Each single module has a conventional ducted-fan configuration and can fly individually. For the single module and the connected array, kinematic and dynamic models are briefly introduced. Based on the derived models, a control system using the sliding mode control (SMC) and proportional-integral-derivative (PID) methods is built into a hierarchical structure. Also, simple kinematics is applied for multiple anti-ship missiles (ASMs) and a target ship. A proportional navigation guidance (PNG) law is designed for the guided missile system. Furthermore, a sequential logic proposed to take account of an expected signal power (ESP) for the deployment strategy. The ESP is calculated by using seeker and decoy signal models at a control station, and then the station sends path planning commands to the multiple decoys. A numerical simulation is conducted under a visualization environment and verifies the decoy mission with two missiles and two decoys. The simulation shows that the separated single modules fulfill the role of the decoy effectively to counteract the multiple ASMs.
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