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Maritime application of ducted-fan flight array system: Decoy for anti-ship missile

机译:管道风扇飞行阵列系统在海上的应用:反舰导弹的诱饵

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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.
机译:本文提出了一种使用导管风扇飞行阵列系统的诱饵应用,该系统由多个单个模块组成。每个单个模块都具有常规的管道风扇配置,并且可以单独飞行。对于单个模块和连接的阵列,简要介绍了运动学模型和动态模型。基于导出的模型,将使用滑模控制(SMC)和比例积分微分(PID)方法的控制系统构建为分层结构。同样,简单的运动学也适用于多种反舰导弹(ASM)和目标舰。针对制导导弹系统设计了比例导航制导(PNG)法。此外,提出了一种顺序逻辑,以考虑部署策略的预期信号功率(ESP)。通过在控制站上使用搜寻器和诱饵信号模型来计算ESP,然后该站将路径规划命令发送到多个诱饵。在可视化环境下进行了数值模拟,并用两个导弹和两个诱饵验证了诱饵任务。仿真表明,分离的单个模块有效地发挥了诱饵的作用,以抵消多个ASM。

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