Notice: Undefined index: linkPowrot in C:\wwwroot\wwwroot\publikacje\publikacje.php on line 1275
[88910] Artykuł: PRE-PROGRAMMED FLIGHT PATH OF AIR-TO-GROUND MISSILECzasopismo: 24th International Conference Engineering Mechanics 2018 Strony: 261-264ISSN: 1805-8256 ISBN: 978-80-86246-91-8 Wydawca: ACAD SCI CZECH REPUBLIC, INST THEORETICAL & APPLIED MECHANICS, PROSECKA 76, PRAGUE 9, 190 00, CZECH REPUBLIC Opublikowano: 2018 Seria wydawnicza: Engineering Mechanics Autorzy / Redaktorzy / Twórcy Grupa MNiSW: Materiały z konferencji międzynarodowej (zarejestrowane w Web of Science) Punkty MNiSW: 15 Klasyfikacja Web of Science: Proceedings Paper DOI Web of Science Keywords: missile  pre-programmed trajectory  guidance  control  dynamics  |
The paper reports a control algorithm for air-to-ground missile that performs a pre-programmed flight along an ellipse section. The control system of the object flight is based on classical PD controllers. The efficiency of the system that guides the missile onto a ground target was analysed. The paper presents selected results of numerical simulations obtained using Matlab/Simulink package.