Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1714324 | Acta Astronautica | 2015 | 17 Pages |
Abstract
UWE-3 introduces also a modular and flexible pico-satellite bus as a robust and extensible base for future missions. Technical objective was a very low power consumption of the COTS-based system, nevertheless providing a robust performance of this miniature satellite by advanced microprocessor redundancy and fault detection, identification and recovery software. This contribution addresses the UWE-3 design and mission results with emphasis on the operational experiences of the attitude determination and control system.
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Engineering
Aerospace Engineering
Authors
S. Busch, P. Bangert, S. Dombrovski, K. Schilling,