Guido Bedin
Design of Robust Control Techniques for a Small Satellite with Flexible Appendages.
Rel. Elisa Capello. Politecnico di Torino, Corso di laurea magistrale in Ingegneria Aerospaziale, 2020
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Abstract
In the latest years, small satellites are becoming more and more utilised by space agencies, thanks to their reduced costs. The technological improvement and the large choice of Components of the Shelf, allowed the space industry to develop smaller and cheaper satellites, able to operate in different missions and scenarios. Due to their limited mass and volume, they can be launched simultaneously with only one launcher, cutting enormously the launch costs. They can be disposed as a constellation and provide services for communications, Earth observation, science experiments or debris removal. All these aspects allowed the non-governmental companies and universities to have access to the space, improving the research of reliable and increasingly smaller satellites, like CubeSats.
Another important characteristic of these satellites is the presence of deployable appendages, like solar arrays, space manipulators, antennas or debris capture systems, to perform different missions and reduce the launch volume
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