A missile guidance law tolerant to unestimated evasive maneuvers

Marzat Julien

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A missile guidance law tolerant to unestimated evasive maneuvers

机译：导弹制导法容忍无法估计的规避演习

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摘要

Purpose - This note aims to introduce a terminal guidance law that is able to compensate for evasive target maneuvers without estimating their acceleration.

机译：目的-本说明旨在介绍一种终极制导律，该律能够补偿逃避的目标机动而无需估计其加速度。

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来源
《Aircraft Engineering and Aerospace Technology》 |2017年第2期|314-319|共6页
作者
Marzat Julien;
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作者单位

Off Natl Etud & Rech Aerosp, Palaiseau, France;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类
关键词
Optimal control; Missile guidance; Proportional navigation; Target maneuver;

机译：最优控制;导弹制导;比例导航;目标机动;

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专利

1. Guidance Synthesis for Evasive Maneuver of Anti-Ship Missiles Against Close-In Weapon Systems [J] . Kim Yoon-Hwan, Ryoo Chang-Kyung, Tahk Min-Jea Aerospace and Electronic Systems, IEEE Transactions on . 2010,第3期

机译：防空导弹对近程武器系统回避机动的制导综合
2. A New Optimal Guidance Law for Air-to-Air Missiles against Evasive Targets [J] . By Lu-Ping Tsao, Ching-Show Lin Transactions of the Japan society for aeronautical and space sciences . 2000,第140期

机译：空空导弹对逃避目标的新的最佳制导律
3. Robust Nonlinear Disturbance Observer Based Adaptive Guidance Law Against Uncertainties in Missile Dynamics and Target Maneuver [J] . Dongkyoung Chwa Aerospace and Electronic Systems, IEEE Transactions on . 2018,第4期

机译：基于鲁棒非线性扰动观测器的导弹动力学和目标机动不确定性自适应制导律
4. A GUIDANCE LAW WITH SINUSOIDAL EVASIVE MANEUVER FOR ENHANCING SURVIVABILITY OF ANTI-SHIP MISSILES [C] . Jin-Ik Lee, Chang-Kyung Ryoo, Keeyoung Choi IFAC Symposium on Automatic Control in Aerospace . 2009

机译：具有正弦疏散机动的指导法，提高防船导弹的生存能力
5. Optimal and near-optimal medium range air-to-air missile guidance against maneuvering targets. [D] . Kumar, Renjith R. 1989

机译：针对机动目标的最佳和近乎最佳的中程空空导弹制导。
6. Terminal attack trajectories of peregrine falcons are described by the proportional navigation guidance law of missiles [O] . Caroline H. Brighton, Adrian L. R. Thomas, Graham K. Taylor 2017

机译：游击猎鹰的终末攻击轨迹由导弹的比例导航制导定律描述
7. Impact Angle Control Guidance Synthesis for Evasive Maneuver against Intercept Missile [O] . Y. H. Yogaswara, Seong-Min Hong, Min-Jea Tahk, 2017

机译：冲击角度控制引导综合对拦截导弹的回避机动

A missile guidance law tolerant to unestimated evasive maneuvers

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