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 recent years, the complexity of CubeSat missions has been increasing steadily as the
platform capabilities have drastically improved. Missions involving high-accuracy pointing …

We consider the problem of attitude stabilization for a low Earth orbit satellite having only
electromagnetic actuation. Such a satellite is not fully actuated, as the control torque is the …

This paper addresses a novel Constrained Magnetic Linear Quadratic Regulator (CM-LQR)
scheme that generates a control torque vector on a plane approximately perpendicular to …

This study is aimed at addressing the practical challenges of conducting hardware-in-the-
loop simulation (HILS) for a CubeSat attitude determination and control system (ADCS) with …

This paper presents the mission analysis of 3Cat-8, a 6-Unit CubeSat mission being
developed by the UPC NanoSat Lab for ionospheric research. The primary objective of the …

CONASAT is being designed to gather environmental data like rain volume, temperature,
humidity, air pollution, ocean streams, environmental hazards, etc. collected and transmitted …

Magnetorquers are a very suitable solution for the nanosatellite's attitude and orbital control
of low Earth orbit (LEO) given its constraints: small available volume, limited power …

The attitude regulation problem with bounded control for a class of satellites in the presence
of large disturbances, with bounded moving average, is solved using a Lyapunov-like …

Exploration of asteroids and small-bodies can provide valuable insight into the origins of the
solar system, into the origins of Earth and the origins of the building blocks of life. However …