جلد 4، شماره 3 - ( 7-1387 )                   جلد 4 شماره 3 صفحات 115-126 | برگشت به فهرست نسخه ها


XML Print


Download citation:
BibTeX | RIS | EndNote | Medlars | ProCite | Reference Manager | RefWorks
Send citation to:

A. Moharampour, J. Poshtan, A. Khaki-Sedigh. A Modified Proportional Navigation Guidance for Range Estimation. IJEEE. 2008; 4 (3) :115-126
URL: http://ijeee.iust.ac.ir/article-1-72-fa.html
محرم پور ، پشتان ، خاکی صدیق . A Modified Proportional Navigation Guidance for Range Estimation. . 1387; 4 (3) :115-126

URL: http://ijeee.iust.ac.ir/article-1-72-fa.html


چکیده:   (7355 مشاهده)

In this paper, after defining pure proportional navigation guidance in the 3-

dimensional state from a new point of view, range estimation for passive homing missiles is

explained. Modeling has been performed by using line of sight coordinates with a particular

definition. To obtain convergent estimates of those state variables involved particularly in

range channel and unavailable from IR trackers, nonlinear filters such as sequential U-D

extended Kalman filter and Unscented Kalman filter in modified spherical coordinate

combined with a modified proportional navigation guidance law are proposed. Simulation

results indicate that the proposed tracking filters in conjunction with the dual guidance law

are able to provide the convergence of the range estimate for both maneuvering and nonmaneuvering

targets.

متن کامل [PDF 322 kb]   (2377 دریافت)    
نوع مطالعه: Research Paper |
دریافت: ۱۳۸۷/۸/۱۸

ارسال نظر درباره این مقاله : نام کاربری یا پست الکترونیک شما:
کد امنیتی را در کادر بنویسید

کلیه حقوق این وب سایت متعلق به می باشد.

طراحی و برنامه نویسی : یکتاوب افزار شرق

© 2015 All Rights Reserved | Iranian Journal of Electrical and Electronic Engineering

Designed & Developed by : Yektaweb