Rela-time midcourse guidance robust to missile launch conditioons

机译：实时中途制导对导弹发射条件具有鲁棒性

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In this paper, an rela-time suboptimal midcourse guidance law robust to missile launch conditions, which is a neural network approximation of the optimal feedback stragegy, is proposed. It is obtained by the appropriate representation of input data of the neural network, which guarantees robustness. Computer simulations show that the proposed guidance law alows the missile to intercept a given target almost exactly with only a limited number of the neural network weights.

机译：本文提出了一种对导弹发射条件具有鲁棒性的相对时间次优中段制导律，即最优反馈策略的神经网络近似。它是通过神经网络输入数据的适当表示而获得的，从而保证了鲁棒性。计算机仿真表明，拟议的制导律允许导弹仅在有限数量的神经网络权重下几乎完全拦截给定目标。

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来源
《4th IFAC(International Federation of Automatic Control) Symposium on Automatic Control in Aerospace 1998 Seoul, Korea, 24-28 August 1998》|1998年|p.111-115|共5页
会议地点 Seoul(KR)
作者
Eun-Jung Song; Min-jea Tahk;
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原文格式 PDF
正文语种 eng
中图分类航空、航天技术的研究与探索;
关键词
guidance systems; suboptimal control; input elements; robustness; neural;

机译：指导系统；次优控制；输入元素；健壮性神经的;

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专利

1. Real-time midcourse missile guidance robust against launch conditions [J] . Eun-Hung Song, Min-Jea Tahk Control Engineering Practice . 1999,第4期

机译：实时中段导弹制导对发射条件具有鲁棒性
2. Optimal midcourse guidance of an air-to-air missile via SVM and RVM [J] . Mortazavi Mohammad Reza, Almasganj Farshad Soft computing: A fusion of foundations, methodologies and applications . 2019,第15期

机译：通过SVM和RVM的空对空气导弹的最佳中流指导
3. Observer-Based Optimal Zero-Sliding Midcourse Guidance for Missiles with TVC and DCS [J] . Fu-Kuang Yeh, Kuang-Yang Kou Transactions of the Japan society for aeronautical and space sciences . 2013,第1期

机译：具有TVC和DCS的导弹基于观测器的最佳零滑行中段制导
4. Rela-time midcourse guidance robust to missile launch conditioons [C] . Eun-Jung Song, Min-jea Tahk International Federation of Automatic Control symposium on automatic control in aerospace . 1999

机译：实时中等地区指导对导弹发射条件强大
5. Short-range, surface-to-surface missile guidance for nonlinear, time-varying target state estimation and missile dynamics. [D] . Frank, Terry Alan. 1995

机译：短程地对地导弹制导，用于非线性，时变目标状态估计和导弹动力学。
6. Research on the Rapid and Accurate Positioning and Orientation Approach for Land Missile-Launching Vehicle [O] . Kui Li, Lei Wang, Yanhong Lv, 2015

机译：陆空导弹发射车快速准确的定位定向方法研究
7. Error Analysis Study on the Veering of Marine Target and the Midcourse Guidance of Anti-ship Missile [O] . In-Soo Kim 2020

机译：海洋目标转向的误差分析与反舰导弹中的中等指导

Rela-time midcourse guidance robust to missile launch conditioons

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