Implementation of the data analysis compilation interface in a satellite monitoring simulator

Cubesat are now widespread as affordable tools for teaching and researching for Universities and Research Centers. Although they are simple platforms, their complexity can be increased in a budget. One of the elements that increase the capabilities of cubesats is the incorporation of an attitude (and orbit) control system (AOCS). Simulation of the capability of these subsystems is the first step to assess the convenience to include such subsystems in a platform.