Modification of the exact pole placement method and its application for the control of spacecraft motion

DOI10.1134/S1064230713020135zbMath1307.93172MaRDI QIDQ2263439

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

Publication date: 18 March 2015

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

Mathematics Subject Classification ID

Variable mass, rockets (70P05) Pole and zero placement problems (93B55)

Related Items (11)

Delayed feedback stabilization and the Huijberts-Michiels-Nijmeijer problem ⋮ Spacecraft attitude control with simultaneous unloading of the angular momentum of inertial actuators ⋮ Unnamed Item ⋮ Asymptotic behavior of solutions of Lorenz-like systems: analytical results and computer error structures ⋮ Output control of the longitudinal motion of a flying vehicle ⋮ Terminal synthesis of orbital orientation for a spacecraft ⋮ Terminal bang-bang impulsive control of linear time invariant dynamic systems ⋮ Output control of a spacecraft motion spectrum ⋮ Algorithms for the synthesis of observers for nonlinear dynamic systems ⋮ Stabilization of coupled motions of an aircraft in the pitch-yaw channels in the absence of information about the sliding angle: analytical synthesis ⋮ Application of generalized Butterworth polynomials for stabilization of the equilibrium position of a space station

Cites Work

• Unnamed Item
• Unnamed Item
• Synthesis of stabilizing spacecraft control based on generalized Ackermann's formula
• Generalized inverses. Theory and applications.
• Identification of the position of an equilibrium attitude of the international space station as a problem of stable matrix completion

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