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...
Hlavní autoři: | , , , , |
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Médium: | Článek |
Jazyk: | English |
Vydáno: |
MDPI AG
2022-01-01
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Edice: | Energies |
Témata: | |
On-line přístup: | https://www.mdpi.com/1996-1073/15/1/356 |