Publikationsdatum:
2019-07-13
Beschreibung:
In this paper, an approach to increase the degree of autonomy of flight software is proposed. We describe an enhancement of the Attitude Determination and Control System by augmenting it with self-calibration capability. Conventional attitude estimation and control algorithms are combined with higher level decision making and machine learning algorithms in order to deal with the uncertainty and complexity of the problem.
Schlagwort(e):
Spacecraft Instrumentation
Materialart:
Flight Mechanics; May 18, 1999 - May 19, 1999; Greenbelt, MD; United States
Format:
text
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