The Possibilities and Usage of Missile Path Mathematical Modelling for the Utilization in Future Autonomous Air Defense Systems Simulators

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F20%3A00555719" target="_blank" >RIV/60162694:G43__/20:00555719 - isvavai.cz</a>

Výsledek na webu

<a href="https://www.springer.com/series/558" target="_blank" >https://www.springer.com/series/558</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1007/978-3-030-43890-6_20" target="_blank" >10.1007/978-3-030-43890-6_20</a>

Jazyk výsledku

angličtina

Název v původním jazyce

The Possibilities and Usage of Missile Path Mathematical Modelling for the Utilization in Future Autonomous Air Defense Systems Simulators

Popis výsledku v původním jazyce

The missile guidance system is one of the most important component of a missile itself and it should be reflected also in a simulation environment. Therefore, the tactical simulators should contain as precise missile models as possible. Unfortunately, the most of contemporary simulators use just a very simplified mathematical models. To bring the simulation closer to the reality the model of each missile should work according to a specific guidance method containing a real guidance equations. The article focuses on the creation and implementation of specific missile characteristics into a tactical simulation environment and outlines its usage for the future simulator of an autonomous air defense system.

Název v anglickém jazyce

The Possibilities and Usage of Missile Path Mathematical Modelling for the Utilization in Future Autonomous Air Defense Systems Simulators

Popis výsledku anglicky

The missile guidance system is one of the most important component of a missile itself and it should be reflected also in a simulation environment. Therefore, the tactical simulators should contain as precise missile models as possible. Unfortunately, the most of contemporary simulators use just a very simplified mathematical models. To bring the simulation closer to the reality the model of each missile should work according to a specific guidance method containing a real guidance equations. The article focuses on the creation and implementation of specific missile characteristics into a tactical simulation environment and outlines its usage for the future simulator of an autonomous air defense system.

Druh

D - Stať ve sborníku

CEP obor

—

OECD FORD obor

20205 - Automation and control systems

Projekt

—

Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2020

Kód důvěrnosti údajů

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

Název statě ve sborníku

Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics)

ISBN

978-3-030-43890-6

ISSN

0302-9743

e-ISSN

1611-3349

Počet stran výsledku

9

Strana od-do

253-261

Název nakladatele

Springer

Místo vydání

Cham, Switzerland

Místo konání akce

Palermo, the Republic of Italy

Datum konání akce

29. 10. 2019

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

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