Synthesis of decoupling laws for controlling the angular motion of landing module with solid-fuel landing engine minimizing the transient time

DOI10.1134/S1064230713030179zbMath1278.93126OpenAlexW2107269036MaRDI QIDQ393690

E. A. Mikrin, A. V. Lapin, N. E. Zubov

Publication date: 23 January 2014

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1064230713030179

zbMATH Keywords

angular velocityminimal transient timelanding moduleangular motionexact pole placement methodmodal controlsolid-fuel landing enginetransient time application

Mathematics Subject Classification ID

Variable mass, rockets (70P05) Pole and zero placement problems (93B55) Synthesis problems (93B50) Control/observation systems governed by ordinary differential equations (93C15)

Cites Work

• Control of angular motion of a landing module of ``Soyuz type upon satellite returning from the orbit
• Synthesis of decoupling laws for attitude stabilization of a spacecraft
• Unnamed Item

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