| Resumen |
In the development of satellite systems, rigorous validation of constituent subsystems is imperative. Among the various subsystems that compose a satellite, the Attitude Determination and Control Sys- tem (ADCS) plays a crucial role in maintaining satellite orientation and stability. The validation process for these subsystems traditionally employs test benches capable of simulating space environment conditions. However, simulating such an environment presents numerous challenges, a significant one being the imbalance caused by the discrepancy between the satellite’s center of mass and its geometric center, which can substantially affect test conditions and results. This work presents a simplified design of a singleaxis balancing system for a 1U CubeSat ADCS testbed. The system utilizes a fuzzy controller designed to operate a sliding mass, which corrects internal system perturbations for the initial configurations of satellite tests. |
