Synthesis of decoupling laws for attitude stabilization of a spacecraft

DOI10.1134/S1064230711060189zbMath1307.93170OpenAlexW1982550070MaRDI QIDQ2263388

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

Publication date: 18 March 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/s1064230711060189

Mathematics Subject Classification ID

Linearizations (93B18) Pole and zero placement problems (93B55) Control/observation systems governed by ordinary differential equations (93C15) Stability of control systems (93D99)

Related Items

Spacecraft attitude control with simultaneous unloading of the angular momentum of inertial actuators ⋮ Synthesis of decoupling laws for controlling the angular motion of landing module with solid-fuel landing engine minimizing the transient time ⋮ Stability analysis of mechanical systems with highly nonlinear positional forces under distributed delay ⋮ Synthesis of spacecraft covariance controls ⋮ Output control of the longitudinal motion of a flying vehicle ⋮ Solvability conditions of problem of synthesizing proportional-integral control of a linear MIMO system ⋮ Methods for the vibration determination and parameter identification of spacecraft with flexible structures ⋮ Terminal synthesis of orbital orientation for a spacecraft ⋮ Synthesis of controls for a spacecraft that optimize the pole placement of the closed-loop control system ⋮ 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 ⋮ Finite eigenvalue assignment for a descriptor system

Cites Work

• Unnamed Item
• Unnamed Item
• 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
• The band formula for A.N. Krylov's problem
• Reduction of the Rosenbrock matrix in analysis of invariant zeros of the linear MIMO-system
• Linear multivariable control. A geometric approach
• Superstable linear control systems. II: Design
• Synthesis of linear quadratic control laws on basis of linear matrix inequalities
• A direct computation of state deadbeat feedback gains
• Robust pole assignment in linear state feedback
• Optimal pole-placement for linear multi-input controllable systems
• A simple solution to the optimal eigenvalue assignment problem