Control Analysis with Modified LQR Method of Anti-Tank Missile with Vectorization of the Rocket Engine Thrust

This article approaches the issue of the optimal control of a hypothetical anti-tank guided missile (ATGM) with an innovative rocket engine thrust vectorization system. This is a highly non-linear dynamic system; therefore, the linearization of such a mathematical model requires numerous simplificat...

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Hlavní autoři: Łukasz Nocoń, Marta Grzyb, Piotr Szmidt, Zbigniew Koruba, Łukasz Nowakowski
Médium: Článek
Jazyk:English
Vydáno: MDPI AG 2022-01-01
Edice:Energies
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On-line přístup:https://www.mdpi.com/1996-1073/15/1/356