Terminal control of the trajectory and rotational motion of an active spacecraft during a rendezvous with a passive spacecraft

DOI10.1134/S1064230716030187zbMath1383.93060OpenAlexW2466556983MaRDI QIDQ1743061

N. E. Zubov, V. N. Ryabchenko, E. A. Mikrin, A. S. Oleinik

Publication date: 12 April 2018

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

Full work available at URL: https://doi.org/10.1134/s1064230716030187

zbMATH Keywords

rendezvousterminal controlspacecraftsminimization of the generalized work functionaltrajectory and rotational motion

Mathematics Subject Classification ID

Application models in control theory (93C95) Variable mass, rockets (70P05) Control/observation systems governed by ordinary differential equations (93C15)

Cites Work

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

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