Control algorithms for the active magnetic attitude control systems are covered in the survey.
Three different situations in the magnetic system implementation are considered. First …

Attitude motion of a satellite equipped with magnetic control system is considered. System
comprises of three magnetorquers and one three-axis magnetometer. Satellite is stabilized …

This paper presents a novel robust attitude controller for satellite applications with magnetic
actuation. First, at the kinematical level, a terminal sliding mode (TSM)-based sliding surface …

Four geomagnetic field models are discussed: IGRF, inclined, direct and simplified dipoles.
Geomagnetic induction vector expressions are provided in different reference frames …

Искусственные спутники Земли практически всегда оснащены системой ориентации
для обеспечения требуемого углового движения вокруг своего центра масс. В связи с …

A satellite in a circular Earth orbit is under consideration. The three–axis stabilization of the
satellite in orbital coordinate system with the attitude control system using moments of …

In this paper, the Earth's magnetic field models which are widely used in spacecraft attitude
control applications are modeled and extensively compared with a reference model. The …

Three-axis magnetic control in orbital reference frame is considered. Magnetorquers are the
only actuators and gravitational torque is the only disturbance source. Full attitude …

Magnetic torquers are attitude control devices used in spacecraft systems, and extensive
research has been conducted on the attitude control of such spacecraft systems equipped …

We consider the stabilization of the satellite relative equilibrium in a circular orbit in the
presence of an electrodynamic satellite attitude control system that uses simultaneously the …