The main onboard use of attitudedata in spacecraft are for the Attitude and Orbit Control function. A caracterization of the performance envelope of autonomous star trackers is hence a common problem in the space community. This study was performed to establish theoretical as well as practical envelopes for different tracker philosophies.
|Effective start/end date||01/01/1996 → 09/08/1997|
- Technical University of Denmark (lead)
- California Institute of Technology (Project partner)
- European Space Agency - ESA (Project partner)
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