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 …

REGULUS is an Iodine-based electric propulsion system. It has been designed and
manufactured at the Italian company Technology for Propulsion and Innovation SpA (T4i) …

REGULUS is a propulsion platform for CubeSats. It integrates the Magnetically Enhanced
Thruster (MET) and its subsystems (ie, fluidic line, electronics, and thermo-structural …

The standard purely magnetic attitude control system utilizes three magnetic actuators to
control the spacecraft attitude about three principal axes. Although these actuators are …

REGULUS is a complete electric propulsion unit fed with iodine propellant that is under
development at Technology for Propulsion and Innovation21, an Italian based company …

CubeSats have became a common platform for education and technology demonstration. To
overcome restrictions on CubeSat design, the Attitude Determination and Control System …

(1) Technology for Propulsion and Innovation SpA, Padova, Italy (2) Centre of Studies and
Activities for Space “Giuseppe Colombo”, University of Padova, Padova, Italy (3) Department …

To optimize the geomagnetic reference vector and the solar reference vector calculation
method, this paper proposes a geomagnetic fitting algorithm and simplifies the DE430 …

Micro and small satellites' market is rapidly growing, and its value is estimated to triple in the
next four years. To allow different mission scenarios, the need for an autonomous, reliable …

This work addresses the design and simulation of an Extended Kalman Filter for attitude
determination in a CubeSat using the MATLAB/Simulink platform. The CubeSat is the …