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 …

The problem of attitude stabilization of a small satellite using magnetic actuators is
considered, a review of the existing approaches based on linear and nonlinear control …

The problem of inertial pointing for a spacecraft with magnetic actuators is addressed and an
almost global solution to the problem is obtained by means of static attitude and rate …

The problems of attitude stabilization and disturbance torque attenuation for a small
spacecraft using magnetic actuators is considered and a solution to the problem in terms of …

The problem of Earth-pointing attitude control for a spacecraft with magnetic actuators is
addressed and a novel approach to the problem is proposed, which guarantees almost …

The first task a spacecraft attitude control system must perform after separation from the
launcher is to detumble the spacecraft, ie, to bring it to a final condition with a sufficiently …

A genetic algorithm was used to optimize performance of a fuzzy inference system acting as
a controller for a magnetically actuated CubeSat. A solely magnetically controlled satellite is …

Inertially pointing satellites which use reaction wheels as main actuators for attitude control
are subject to the problem of wheel saturation. This problem can be partially obviated by …

The problem of designing discrete-time attitude controllers for three-axis stabilization of
magnetically actuated spacecraft is considered. Several methods are discussed and an …

The development process for spacecraft control systems relies heavily on modelling and
simulation tools for spacecraft dynamics. For this reason, there is an increasing need for …