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The IR missile (spin-scan and con-scan seekers) countermeasures

机译:红外导弹(自旋扫描和同向扫描导引头)对策

摘要

In the combat scenario where the infrared missile is an almost continuous threat during the operation, fighter aircraft are currently quite susceptible to being killed in attacks by infrared missiles. Theoretical analysis applied to an encounter simulation seems to indicate that it is possible to use the infrared Active Jammer and the expendable decoy (flare) to defeat the infrared missile (spin-scan and con-scan seekers). The theoretical analysis of a simplified case of a spin-scan and con-scan reticle with amplitude modulation, frequency modulation and phase modulation leads to expressions for the targets' positions, as seen by the missile seeker, under no-jamming condition. The signal waveforms consist of target radiation power failing on the reticle and the reticle modulation function. We apply signal processing techniques to the modulated signal to determine the tracking error rate under no-jamming, active jamming and flare jamming different conditions, and by comparing with the unjammed tracking error rate, to determine the differences and effectiveness of jamming. The analytical result is simulated by means of a simulation program (MATLAB), which evaluates the change in the missile LOS (line of sight ) rotation rate and the impact on the missile guidance operation. The analysis indicated successful jamming in the different jamming source situations. Following the jamming analysis, one can use the result to do further operational analysis as in OT&E (operation test and evaluation) and to evaluate the operational effectiveness of the jammers and to develop operational tactics to further increase the survivability of the fighter aircraft in the combat situation.
机译:在作战过程中红外导弹几乎是连续的威胁的战斗场景中,战斗机目前很容易在红外导弹的袭击中丧生。应用于相遇模拟的理论分析似乎表明,可以使用红外主动干扰机和消耗性诱饵(火炬)打败红外导弹(自旋扫描和共扫描搜索头)。对具有调幅,调频和调相的自旋扫描和共扫描掩模版的简化情况进行理论分析,得出了在无干扰条件下导弹导引头看到的目标位置的表达式。信号波形由分划板上的目标辐射功率和分划板调制功能组成。我们将信号处理技术应用于调制信号,以确定在无干扰,主动干扰和火炬干扰不同条件下的跟踪误差率,并与未干扰的跟踪误差率进行比较,以确定干扰的差异和有效性。分析结果通过模拟程序(MATLAB)进行模拟,该程序评估导弹LOS(视线)旋转速率的变化以及对导弹制导操作的影响。分析表明在不同的干扰源情况下成功进行了干扰。进行干扰分析之后,可以像OT&E(操作测试和评估)中那样,使用结果进行进一步的作战分析,评估干扰机的作战效能并制定作战策略,以进一步提高战斗机在战斗中的生存能力情况。

著录项

  • 作者

    Chang Ting Li;

  • 作者单位
  • 年度 1994
  • 总页数
  • 原文格式 PDF
  • 正文语种 en_US
  • 中图分类

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