Proceedings Vol. 22 (2016)
ENGINEERING MECHANICS 2016
May 9 – 12, 2016, Svratka, Czech Republic
Copyright © 2016 Institute of Thermomechanics, Academy of Sciences of the Czech Republic, v.v.i., Prague
ISSN 1805-8248 (printed)
ISSN 1805-8256 (electronic)
list of papers scientific commitee
pages 193 - 196, full text
The paper analyzes a possibility of using the special algorithm to control the flight of a homing air target missile. The method is based on the signum function and utilizes the phase trajectories of errors resulting from the adopted homing method (proportional navigation). The results obtained via Matlab package are presented in graphical form.
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All papers were reviewed by members of the scientific committee.