Synthesis of spacecraft covariance controls

DOI10.1134/S1064230714060136zbMath1327.93365OpenAlexW2080989933MaRDI QIDQ895307

N. E. Zubov, V. N. Ryabchenko, M. Sh. Misrikhanov

Publication date: 27 November 2015

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

Full work available at URL: https://doi.org/10.1134/s1064230714060136

Mathematics Subject Classification ID

Stabilization of systems by feedback (93D15) Variable mass, rockets (70P05) Synthesis problems (93B50) Stochastic systems in control theory (general) (93E03)

Related Items (1)

Synthesis of linear postcompensators for signal processing of nonlinear systems of a special form

Cites Work

• Unnamed Item
• Unnamed Item
• Synthesis of stabilizing spacecraft control based on generalized Ackermann's formula
• Unloading angular momentum for inertial actuators of a spacecraft in the pitch channel
• Pole placement in large dynamical systems with many inputs and outputs
• Synthesis of decoupling laws for attitude stabilization of a spacecraft
• Synthesis of controls for a spacecraft that optimize the pole placement of the closed-loop control system
• Covariance control theory
• A direct computation of state deadbeat feedback gains
• A simple solution to the optimal eigenvalue assignment problem

This page was built for publication: Synthesis of spacecraft covariance controls