Simulation of short range missile guidance using proportional navigation

机译：使用比例导航模拟短程导弹指导

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This article presents proportional navigation(PN) and its few variants used in modern tactical missile guidance. This article develops 6-DOF mathematical model and an autopilot for PN guided missile. Full Simulink simulation and animation of PN navigation in three dimensions is shown and discussed.

机译：本文提出了现代战术导弹指导中使用的比例导航（PN）及其几种变体。本文开发了6- DOF数学模型和PN引导导弹的自动驾驶仪。显示并讨论了三维PN导航的完整Simulink仿真和动画。

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《International Symposium INFOTEH-JAHORINA》|2021年|1-6|共6页
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Mirza Hodžić; Naser Prljača;
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Navigation; Software packages; Missile guidance; Autopilot; Mathematical model; Acceleration; Matlab;

机译：导航;软件包;导弹指导;自动驾驶仪;数学模型;加速;matlab;

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专利

1. A novel robust proportional navigation guidance law design for missile considering autopilot dynamic [J] . Seyyed Sajjad Moosapour, Ghasem Alizadeh, Sohrab Khanmohammadi, Transactions of the Institute of Measurement and Control . 2013,第5期

机译：考虑自动驾驶动态的新型鲁棒比例导航制导律设计
2. Short-time stability of proportional navigation guidance loop [J] . Dong-Young Rew, Min-Jea Tahk, Hangju Cho IEEE Transactions on Aerospace and Electronic Systems . 1996,第3期

机译：比例导航制导环的短时稳定性
3. Short-time stability of proportional navigation guidance loop [J] . Dong-Young Rew, Min-Jea Tahk IEEE Transactions on Aerospace and Electronic Systems . 1996,第3期

机译：比例导航制导环的短时稳定性
4. Multiple Missiles Cooperative Guidance Based on Proportional Navigation Guidance [C] . Qiangqiang Xu, Jianquan Ge, Tao Yang Chinese Control and Decision Conference . 2020

机译：基于比例导航的多导弹协同制导
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. 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. Performance Comparisons between Command to Line-of-Sight Guidance Law and Proportional Navigation Guidance Law in Short Range Surface-to-Air Missile [O] . 2007

机译：在短程面对空中导弹中指挥对视线指导法的绩效比较和比例导航指导法
8. Maximum Launch Range For an Air-to-Air Missile Employing Proportional Navigation for Guidance. [R] . graves,timothy j. 1974

机译：使用比例导航进行制导的空空导弹的最大发射范围。

Simulation of short range missile guidance using proportional navigation

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