Modeling missile flight characteristics by estimating mass and ballistic parameters

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F19%3A00535381" target="_blank" >RIV/60162694:G43__/19:00535381 - isvavai.cz</a>

Výsledek na webu

<a href="http://aimt.unob.cz//articles/19_01/1247.pdf" target="_blank" >http://aimt.unob.cz//articles/19_01/1247.pdf</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.3849/aimt.01247" target="_blank" >10.3849/aimt.01247</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Modeling missile flight characteristics by estimating mass and ballistic parameters

Popis výsledku v původním jazyce

This paper deals with one of the possible methods of a qualified estimation of tactical and technical parameters of surface-to-air or air-to-air guided missiles. This method is designed to estimate missile flight parameters in case of they are unavailable from public sources. Although the method does not provide exact values, it is sufficient for modeling and subsequent simulation. This method is based on the use of so-called "characteristic numbers" of the missile and on assumption of validity of the hypothesis about the similarity of characteristic missile numbers equal or, respectively, similar technological levels. To validate the obtained parameters, a method of mathematical modeling of the missile guidance process is used. The method can also be used for a qualified estimation of missile parameters in the case of an acquisition process.

Název v anglickém jazyce

Modeling missile flight characteristics by estimating mass and ballistic parameters

Popis výsledku anglicky

This paper deals with one of the possible methods of a qualified estimation of tactical and technical parameters of surface-to-air or air-to-air guided missiles. This method is designed to estimate missile flight parameters in case of they are unavailable from public sources. Although the method does not provide exact values, it is sufficient for modeling and subsequent simulation. This method is based on the use of so-called "characteristic numbers" of the missile and on assumption of validity of the hypothesis about the similarity of characteristic missile numbers equal or, respectively, similar technological levels. To validate the obtained parameters, a method of mathematical modeling of the missile guidance process is used. The method can also be used for a qualified estimation of missile parameters in the case of an acquisition process.

Druh

J_SC - Článek v periodiku v databázi SCOPUS

CEP obor

—

OECD FORD obor

20205 - Automation and control systems

Projekt

—

Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2019

Kód důvěrnosti údajů

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

Název periodika

Advances in Military Technology

ISSN

1802-2308

e-ISSN

2533-4123

Svazek periodika

14

Číslo periodika v rámci svazku

1

Stát vydavatele periodika

CZ - Česká republika

Počet stran výsledku

11

Strana od-do

47-57

Kód UT WoS článku

—

EID výsledku v databázi Scopus

2-s2.0-85072107304