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[87660] Artykuł: Analysis of gyroscope system sliding mode control in a target seeking and tracking processCzasopismo: Zamm-zeitschrift Fur Angewandte Mathematik Und Mechanik Tom: 99, Zeszyt: 4, Strony: 1-17ISSN: 0044-2267 Wydawca: WILEY-V C H VERLAG GMBH, POSTFACH 101161, 69451 WEINHEIM, GERMANY Opublikowano: 2019 Autorzy / Redaktorzy / Twórcy Grupa MNiSW: Publikacja w czasopismach wymienionych w wykazie ministra MNiSzW (część A) Punkty MNiSW: 70 Klasyfikacja Web of Science: Article; Proceedings Paper DOI Web of Science Keywords: gyroscope system  sliding mode controller  target seeking and tracking   |
The task of a homing head of an anti-aircraft short-range missile is to determine the position of the missile relative to a target. The most modern missiles use scanning heads. The propelling element of such a head in the paper is a gyroscope system. Disturbance acting on a gyroscope system cause its deviations from the set direction. In order to ensure precise and stable target tracking by a head, it is important to optimally select the gyroscope system control parameters, which enables mitigating the impact of such disturbance on the positioning accuracy of its axis. The paper suggests and implements a sliding mode controller in a gyroscope system, used for target seeking and tracking. Tests comparing a control system with a PD controller with optimal parameters and with a sliding mode controller were performed in a Matlab/Simulink environment. Selected test results were shown in graphic form.