Development and Implementation of a Mass Balancing System for CubeSat Attitude Hardware-in-the-Loop Simulations
Spacecraft simulator platforms can simulate the microgravity environment of space on Earth, for the purposes of testing the Attitude and Orbit Control Subsystem of satellites. In order to do this, the satellite is mounted on a bench and the combined center of mass of this assembly is controlled by a...
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| Format: | Others |
| Language: | English |
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Luleå tekniska universitet, Rymdteknik
2019
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-72351 |