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A new homing guidance law to reduce sensitivity on initial heading errors

机译:新的寻的制导律,以减少对初始航向误差的敏感性

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摘要

In this paper, a new guidance law is developed to reduce sensitivity on heading errors at the initial homing phase. The key enabler to propose such a guidance law was to design a new performance index by introducing distribution functions to the input weighting. The distribution functions in the new performance index are expressed in terms of a second-order polynomial of time-to-go and inverse weighted time-to-go. This allows distribution of the relative input weighting over the entire homing phase. Then, a homing guidance law is derived by applying the optimal control theory to the linear quadratic optimal problem with the new performance index. Unlike the conventional proportional navigation (PN) guidance law with a constant navigation gain, the proposed guidance law has a time-varying gain to ease the heading error sensitivity at the initial homing phase. The characteristics of the proposed guidance algorithm are analytically investigated and its performance is demonstrated through numerical simulations.
机译:在本文中,开发了一种新的制导律,以降低初始归位阶段对航向误差的敏感性。提出这种指导法则的关键因素是通过在输入权重中引入分布函数来设计新的绩效指标。新的性能指标中的分布函数用走时的二阶多项式和走时的逆加权来表示。这允许在整个归位阶段分配相对输入权重。然后,通过将最优控制理论应用于具有新性能指标的线性二次最优问题,推导了寻的制导律。与具有恒定导航增益的常规比例导航(PN)制导律不同,所提出的制导律具有随时间变化的增益,以减轻初始归位阶段的航向误差敏感性。对提出的制导算法的特点进行了分析研究,并通过数值仿真证明了其性能。

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