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 …

In this paper, a finite-time fault-tolerant control method is developed for attitude tracking of a
nano-satellite with three magnetorquers and one reaction wheel in the presence of actuator …

Small satellites use commercial off-the-shelf sensors and actuators for attitude determination
and control (ADC) to reduce the cost. These sensors and actuators are usually not as robust …

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, an adaptive modified sliding mode control approach is developed for attitude
tracking of a nano-satellite with three magnetorquers and one reaction wheel. A sliding …

The stabilization of the relative equilibrium of a satellite moving in a circular orbit, which is
equipped with magnetic orientation system. It is shown that the linearized system of …

The paper deals with a dynamically symmetric satellite in a circular near-Earth orbit. The
satellite is equipped with an electrodynamic attitude control system based on Lorentz and …

The performance of the attitude motion determination algorithm of the SiriusSat-1
nanosatellite is presented. Onboard magnetometer measurements are used. These …

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 …

This paper is concerned with magnetic attitude control of spacecraft. The operation of the
magnetic actuators is usually on a duty cycle; during the off times in this duty cycle the …