Counter countermeasure method for missile's imaging infrared seeker

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F16%3A00532976" target="_blank" >RIV/60162694:G43__/16:00532976 - isvavai.cz</a>

Result on the web

<a href="http://ieeexplore.ieee.org/document/7778064/" target="_blank" >http://ieeexplore.ieee.org/document/7778064/</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1109/DASC.2016.7778064" target="_blank" >10.1109/DASC.2016.7778064</a>

Result language

angličtina

Original language name

Counter countermeasure method for missile's imaging infrared seeker

Original language description

This paper deals with an elimination of jamming optoelectronic seekers by flares. It is predominantly focused on the design and testing of the method of object discrimination for imaging infrared seeker. To design this method, an analysis of capability of imaging infrared seekers to discriminate objects according to their shape was used. On the basis of the results of this analysis, the principle of object selection by their motion inside the field of view of the coordinator was selected for the design of the method of object discrimination. To test this method, a computer program based on input conditions was created to compute trajectories of aircraft and flares. A further computer program simulating the behavior of the imaging infrared seeker and the missile itself uses information about the trajectory of aircraft and the flares to estimate relative position of those objects and the missile. It also evaluates the position of the entire object within the field of view and chooses a proper object by using the designed method of object discrimination. As an indicator of the success rate of the designed method to properly choose a good target (aircraft), the miss distance was used. On the basis of the achieved miss distances for various initiate relative positions of the missile and the aircraft and for various sequences of the flare dispense with aircraft maneuvers, the decision-making criterion is defined whether the method was successful or not. The evaluation of the success or failure of the method is realized by percentage of failure simulations from all realized ones under given input conditions.

Czech name

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Czech description

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Type

D - Article in proceedings

CEP classification

KA - Militarism

OECD FORD branch

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Project

—

Continuities

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year

2016

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection

IEEE 35th Digital Avionics Systems Conference

ISBN

978-150905600-2

ISSN

2155-7195

e-ISSN

—

Number of pages

8

Pages from-to

1-8

Publisher name

IEEE

Place of publication

IEEE, USA

Event location

Sacramento, California, USA

Event date

Sep 25, 2016

Type of event by nationality

WRD - Celosvětová akce

UT code for WoS article

000390558400118