A Micro Satellite Communication System Architecture

Computer Science

Scientific paper

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Scientific paper

In 2000 the European Space Agency's (ESA) Office for Educational Project Outreach Activities has started the Student Space Exploration &Technology Initiative (SSETI). The main objective of this project is to construct and to launch a microsatellite developed by a network of European students. The microsatellite will be mainly used to transmit pictures of the space to earth, to perform plasma experiments and to test all the subsystems for further missions. The data transfer from on-board the satellite to the ground station will be ensued through an innovative communication system composed of two different channels alternatively used to built a connection with the earth. A low data rate channel has to be activated to download telemetry and upload telecommand during the stabilisation mode or when the satellite is not visible from the earth. During the microsatellite nominal operation mode, pictures and data of scientific interest have to be sent from space to the ground station through an additional high data rate channel. As the satellite operation mode changes, a switching system optimizes the onboard power budget selecting the most convenient option between a directive and an omnidirectional antenna, designed to implement the high and low data rate channels respectively. The low gain channel uses two circular polarised patches while a 2x2 microstrip array has been chosen for realising the high rate communication link. Both the antennas are low profile radiators and they have been designed to be conformally mounted onto the microsatellite surface. Prototypes of the two antennas have been realised and tested. A description of the antenna's design process will be given together with a review of the entire system architecture rationale.

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