POINTING OF CUBESATS WITH AND WITHOUT REACTION WHEELS – COMPARATIVE EFFECTS AND APPLICATION TO THE NANOMIRAX/CRON-1 MISSION
NANOMIRAX is a 2U nanosatellite, whose payload is the X-ray Cosmic Burst Localizer (LECX) experiment, capable of capturing gamma ray bursts (GRB) between 30 and 200 keV with a 53°×53° field of view. For the mission's objectives, the experiment should spend more time pointed at space than at Earth. The satellite is made up of GPS sensors, magnetometers and solar sensors. The objective of this work is to compare the performance of attitude control with magnetorqueators and reaction wheels given the strategies: detumbling and limit zone control. Detumbling aims to reduce the satellite's angular velocity. Limit zone control aims to prevent the experiment from being directed towards Earth and maximizing the search area. Modeling of NANOMIRAX's orbital motion and attitude was validated in numerical simulations. The performance of magnetic actuators was compared in relation to the type of limit zone control strategy, taking into account the magnetization and demagnetization of these equipment. For the reaction wheels the performance was compared in relation to the wheel arrangement with a PD control type.