Notice: Undefined index: linkPowrot in C:\wwwroot\wwwroot\publikacje\publikacje.php on line 1275
Strona główna > Publikacje
Publikacje
Pomoc (F2)
[37204] Artykuł:

An algorithm for selecting optimal controls to determine the estimators of the coefficients of a mathematical model for the dynamics of a self-propelled anti-aircraft missile system

Czasopismo: Proceedings of the Institution of Mechanical Engineers Part K-Journal of Multi-Body Dynamics   Tom: 227, Zeszyt: 1, Strony: 12-16
ISSN:  1464-4193
Wydawca:  SAGE PUBLICATIONS LTD, 1 OLIVERS YARD, 55 CITY ROAD, LONDON EC1Y 1SP, ENGLAND
Opublikowano: 2013
 
  Autorzy / Redaktorzy / Twórcy
Imię i nazwisko Wydział Katedra Procent
udziału		 Liczba
punktów
Zbigniew Koruba orcid logoWMiBMKatedra Technik Komputerowych i Uzbrojenia**5012.50  
Izabela Krzysztofik orcid logoWMiBMKatedra Technik Komputerowych i Uzbrojenia**5012.50  

Grupa MNiSW:  Publikacja w czasopismach wymienionych w wykazie ministra MNiSzW (część A)
Punkty MNiSW: 25
Klasyfikacja Web of Science: Article

DOI LogoDOI     Web of Science Logo Web of Science    
Keywords:

Optimal control  coefficient  dynamics  self-propelled anti-aircraft missile system 


Abstract:

Today’s self-propelled anti-aircraft missile systems are designed to intercept low-flying, manoeuvring targets not only under any weather conditions but also during movement of the carrier vehicle over rough terrain. As target search and tracking need to be reliable, i.e. not affected by unfavorable conditions, a self-propelled surface-to-air missile system requires suitable stabilization and control systems. This implies that it is necessary to develop an adequate mathematical model of the missile system dynamics. In this article, we propose a procedure for experimental design to determine the coefficients of such a model. Particular attention is paid to the algorithm for selecting optimal controls and a time-dependent measurement spectrum to minimize the assumed criterion of quality.


POWRÓT
Strona główna > Publikacje