Proceedings Vol. 25 (2019)
ENGINEERING MECHANICS 2019
May 13 – 16, 2019, Svratka, Czech Republic
Copyright © 2019 Institute of Thermomechanics of the Czech Academy of Sciences, Prague
ISSN 1805-8248 (printed)
ISSN 1805-8256 (electronic)
list of papers scientific commitee
pages 73 - 76, full text
This paper examines a linear-quadratic stabilization system for a canard-controlled missile. An analytical method for selecting the weighting elements of the gain matrix in the feedback loop is also proposed, eliminating the need for an iterative solution to the Riccati equation. The proposed solution was evaluated using simulation tests.
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All papers were reviewed by members of the scientific committee.
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