Terminal bang-bang impulsive control of linear time invariant dynamic systems

DOI10.1134/S1064230714030174zbMath1311.49089MaRDI QIDQ2263914

A. S. Oleinik, V. N. Ryabchenko, M. Sh. Misrikhanov, E. A. Mikrin, N. E. Zubov

Publication date: 19 March 2015

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

zbMATH Keywords

bang-bang impulsive controllinear time invariant dynamic systemsspace vehicles rendezvous

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Existence of optimal solutions belonging to restricted classes (Lipschitz controls, bang-bang controls, etc.) (49J30) Impulsive optimal control problems (49N25)

Related Items (3)

Output control of the longitudinal motion of a flying vehicle ⋮ Terminal control of the trajectory and rotational motion of an active spacecraft during a rendezvous with a passive spacecraft ⋮ Terminal synthesis of orbital orientation for a spacecraft

Cites Work

• Unnamed Item
• The use of the exact pole placement algorithm for the control of spacecraft motion
• Synthesis of decoupling laws for attitude stabilization of a spacecraft
• Modification of the exact pole placement method and its application for the control of spacecraft motion

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