Dynamics of spacecraft with elastic and dissipative elements in the attitude control mode

DOI10.1134/S1064230714050025zbMath1307.93180MaRDI QIDQ2017654

S. S. Krylov, A. S. Filippova, L. D. Akulenko, T. T. Win, Yu. G. Markov

Publication date: 23 March 2015

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

zbMATH Keywords

attitude controlgyrostabilizersrotational motion of a spacecraft

Mathematics Subject Classification ID

Nonlinear systems in control theory (93C10) Variable mass, rockets (70P05) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (2)

Angular motion control of a large space structure with elastic elements ⋮ Controlling the one-dimensional motion of hybrid vibrational rod systems

Cites Work

• On the motion of a solid body with elastic and dissipative elements
• Unnamed Item

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