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首页> 外文期刊>Journal of guidance, control, and dynamics >Capturability of Augmented Pure Proportional Navigation Guidance Against Time-Varying Target Maneuvers
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Capturability of Augmented Pure Proportional Navigation Guidance Against Time-Varying Target Maneuvers

机译:针对时变目标机动的增强纯比例导航制导能力

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摘要

This paper proposes a variation of the pure proportional navigation guidance law, called augmented pure proportional navigation, to account for target maneuvers, in a realistic nonlinear engagement geometry, and presents its capturability analysis. These results are in contrast to most work in the literature on augmented proportional navigation laws that consider a linearized geometry imposed upon the true proportional navigation guidance law. Because pure proportional navigation guidance law is closer to a realistic implementation of proportional navigation than true proportional navigation law, and any engagement process is predominantly nonlinear, the results obtained in this paper are more realistic than any available in the literature. Sufficient conditions on speed ratio, navigation gain, and augmentation parameter for capturability, and boundedness of lateral acceleration, against targets executing piecewise continuous maneuvers with time, are obtained. Further, based on a priori knowledge of the maximum maneuver capability of the target, a significant simplification of the guidance law is proposed in this paper. The proposed guidance law is also shown to require a shorter time of interception than standard pure proportional navigation and augmented proportional navigation. To remove chattering in the interceptor maneuver at the end phase of the engagement, a hybrid guidance law using augmented pure proportional navigation and pure proportional navigation is also proposed. Finally, the guaranteed capture zones of standard and augmented pure proportional navigation guidance laws against maneuvering targets are analyzed and compared in the normalized relative velocity space. It is shown that the guaranteed capture zone expands significantly when augmented pure proportional navigation is used instead of pure proportional navigation. Simulation results are given to support the theoretical findings.
机译:本文提出了一种纯比例导航制导律的变体,称为增强型纯比例导航,以解决实际非线性啮合几何中的目标机动问题,并提出了其可捕获性分析。这些结果与文献中有关比例比例导航定律的大多数工作形成了鲜明对比,后者考虑了施加在真实比例导航制导律上的线性几何。由于纯比例导航制导律比真正的比例导航律更接近于比例导航的实际实现,并且任何参与过程都主要是非线性的,因此本文获得的结果比文献中的任何结果都更现实。获得了速度比,导航增益和可捕获性的扩充参数以及横向加速度有界的充分条件,以应对随时间分段执行连续机动的目标。此外,基于对目标的最大机动能力的先验知识,本文提出了对制导律的显着简化。与标准的纯比例导航和增强比例导航相比,拟议的制导律还要求拦截时间更短。为了消除在交战结束阶段拦截机操纵中的颤动,还提出了一种混合的制导律,它使用了增强的纯比例导航和纯比例导航。最后,在归一化的相对速度空间中对标准和增强的纯比例导航制导律针对机动目标的保证捕获区域进行了分析和比较。结果表明,当使用增强的纯比例导航代替纯比例导航时,保证捕获区域会显着扩展。仿真结果给出了理论上的支持。

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  • 来源
    《Journal of guidance, control, and dynamics 》 |2014年第5期| 1446-1461| 共16页
  • 作者单位

    Indian Institute of Science, Bangalore 560012, India,IISc Mathematics Initiative and Guidance, Control, and Decision Systems Laboratory, Department of Aerospace Engineering;

    Indian Institute of Science, Bangalore 560012, India,Control and Decision Systems Laboratory, Department of Aerospace Engineering;

    Indian Institute of Science, Bangalore 560012, India;

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