Electrodynamic stabilization of artificial Earth satellites in the König coordinate system

DOI10.1134/S1064230716010020zbMath1383.93067OpenAlexW2346254631MaRDI QIDQ1743046

Xianqiang Yang

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/s1064230716010020

zbMATH Keywords

asymptotic stabilityartificial Earth satelliteelectrodynamic stabilizationKönig coordinate systemLorentz and magnetic control torques

Mathematics Subject Classification ID

Nonlinear systems in control theory (93C10) Variable mass, rockets (70P05) Asymptotic stability in control theory (93D20) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (2)

Attitude stabilization of a rigid body under disturbances with zero mean values ⋮ Attitude stabilization of a rigid body in conditions of decreasing dissipation

Cites Work

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• The use of the exact pole placement algorithm for the control of spacecraft motion
• Laboratory study of magnetic properties of hysteresis rods for attitude control systems of minisatellites
• Vibrational stabilization and the Brockett problem
• Monoaxial electrodynamic stabilization of Earth satellite in the orbital coordinate system
• Optimizing the electrodynamical stabilization method for a man-made Earth satellite
• Parametric control in the problem of spacecraft stabilization in the geomagnetic field
• Testing of attitude control algorithms for microsatellite ``Chibis-M at laboratory facility
• Synthesis of controls for a spacecraft that optimize the pole placement of the closed-loop control system
• Analytical solution of the time-optimal slew problem of a spherically symmetric spacecraft in the class of conical motions

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