000022748 001__ 22748 000022748 005__ 20220110134524.0 000022748 04107 $$aeng 000022748 046__ $$k2018-05-14 000022748 100__ $$aGrzyb, M. 000022748 24500 $$aPre-programmed flight path of air-to-ground missile 000022748 24630 $$n24.$$pEngineering Mechanics 2018 000022748 260__ $$bInstitute of Theoretical and Applied Mechanics of the Cech Academy of Sciences, Prague 000022748 506__ $$arestricted 000022748 520__ $$2eng$$aThe 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. 000022748 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb. 000022748 653__ $$amissile, pre-programmed trajectory, guidance, control, dynamics 000022748 7112_ $$aEngineering Mechanics 2018$$cSvratka, CZ$$d2018-05-14 / 2018-05-17$$gEM2018 000022748 720__ $$aGrzyb, M.$$iKoruba, Z. 000022748 8560_ $$ffischerc@itam.cas.cz 000022748 8564_ $$s276630$$uhttps://invenio.itam.cas.cz/record/22748/files/261.pdf$$yOriginal version of the author's contribution in proceedings, page , section MCT. 000022748 962__ $$r21225 000022748 980__ $$aPAPER