Pre-programmed flight path of air-to-ground missile
Abstract eng: 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.
Contributors:
Publisher:
Institute of Theoretical and Applied Mechanics of the Cech Academy of Sciences, Prague
Conference Title:
Conference Title:
Engineering Mechanics 2018
Conference Venue:
Svratka, CZ
Conference Dates:
2018-05-14 / 2018-05-17
Rights:
Text je chráněný podle autorského zákona č. 121/2000 Sb.
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Record created 2022-01-10, last modified 2022-01-10
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