In this paper, a brief overview of the nanosatellite on-board computer (OBC) functions will be described. The main advantages and disadvantages of the most common OBC architecture will be explained. A set of three different architecture variants for TUMnanoSAT series of CubeSat nanosatellites is proposed and described. A feature comparison is performed in order to highlight the improvements and advantages of the proposed on-board computer architecture designs over traditional CubeSat OBC architectures.
In this paper, a brief overview of TUMnanoSAT's educational and scientific missions, the impact on system design and educational opportunities are presented. The main basic test procedures for the launch of this nanosatellite are described, including the structure, power supply and attitude control. The main mission of TUMnanoSAT is to provide practical experience to students not only in designing, building, but also testing the nanosatellite with various missions.
This document will cover the overview, development and implementation of mission control platform for TUMnanoSAT, a CubeSat developed at Technical University of Moldova. A mission control platform is essential for a space mission in order to command and control different subsystems, monitor their health, process telemetry and useful data, receive and control requests but also in presented scenario it should be strongly linked to radio software defined architecture from ground station.
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