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31164

ANALYSIS OF THE ANGLE TRACKING ERROR INDUCED IN A RADAR HOMING MISSILE BY PHASE-FRONT DISTORTED JAMMING

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Last updated: 24 Dec 2024

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Abstract

ABSTRACT
In this paper a general analytical formula for the error induced in an angle tracking system by a phase front distorted jamming is derived. The electric fields originating from two coherent jamming sources are analyzed. The amplitude and phase of their resultant are computed; from which the parameters affecting that field are studied and the phase front equation is derived and plotted for different values of those parameters. Further analysis of the phase front equation leads to studying its inclination to the ideal spherical phase front, which leads to a general formula for the induced angular error. A similar approach was adopted in ref. [5] but the derivation was done in a special case. It is interesting that the resulting angular error depends only on the jamming system parameters and does not depend on the tracking system parameters or even on its type.

DOI

10.21608/asat.2001.31164

Keywords

Proportional navigation, self-protection jamming, phase front, phase-front distortion, cross-eye, angle deception technique, coherent jamming sources

Authors

First Name

ALADIN

Last Name

ASSISI

MiddleName

-

Affiliation

PhD., Egyptian Armed Forces.

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Volume

9

Article Issue

ASAT Conference, 8-10 May 2001

Related Issue

4547

Issue Date

2001-05-01

Receive Date

2019-05-06

Publish Date

2001-05-01

Page Start

1

Page End

10

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_31164.html

Detail API

https://asat.journals.ekb.eg/service?article_code=31164

Order

80

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

ANALYSIS OF THE ANGLE TRACKING ERROR INDUCED IN A RADAR HOMING MISSILE BY PHASE-FRONT DISTORTED JAMMING

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Article

Created At

22 Jan 2023