Control of angular motion of a landing module of ``Soyuz type upon satellite returning from the orbit

DOI10.1134/S1064230711050078zbMath1266.93101MaRDI QIDQ353711

L. I. Komarova, E. A. Mikrin, S. N. Evdokimov, S. I. Klimanov

Publication date: 16 July 2013

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

zbMATH Keywords

mathematical modela-posteriori estimation of balancing characteristicsalgorithms of analog and digital control loopscontrol of angular motionlanding module

Mathematics Subject Classification ID

Automated systems (robots, etc.) in control theory (93C85) Variable mass, rockets (70P05)

Related Items (3)

History of spacecraft control systems ⋮ Synthesis of decoupling laws for controlling the angular motion of landing module with solid-fuel landing engine minimizing the transient time ⋮ Correction of a strapdown inertial navigation system during descent in the atmosphere

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