000022695 001__ 22695
000022695 005__ 20220110134521.0
000022695 04107 $$aeng
000022695 046__ $$k2018-05-14
000022695 100__ $$aBaranowski, L.
000022695 24500 $$aAnalysis of two-channel control according to the proportional navigation method

000022695 24630 $$n24.$$pEngineering Mechanics 2018
000022695 260__ $$bInstitute of Theoretical and Applied Mechanics of the Cech Academy of Sciences, Prague
000022695 506__ $$arestricted
000022695 520__ $$2eng$$aIn this paper the equations of the ideal constraints of the proportional navigation method have been presented, as well as the simplified equations applicable in two-channel anti-aircraft missile control. Using the elaborated mathematical model of homing the test missile some numerical experiments have been conducted, regarding the influence of the undertaken simplification in realisation of the homing method constrains on the flight dynamics and the hit accuracy of the canard configuration rocket.

000022695 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000022695 653__ $$ahoming guidance, control systems, proportional navigation, programme constraints

000022695 7112_ $$aEngineering Mechanics 2018$$cSvratka, CZ$$d2018-05-14 / 2018-05-17$$gEM2018
000022695 720__ $$aBaranowski, L.
000022695 8560_ $$ffischerc@itam.cas.cz
000022695 8564_ $$s828659$$uhttps://invenio.itam.cas.cz/record/22695/files/049.pdf$$yOriginal version of the author's contribution in proceedings, page , section MCT.
000022695 962__ $$r21225
000022695 980__ $$aPAPER