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Optimized state-dependent Riccati Equation method for spacecraft attitude estimation and control

Conference Paper (2012)
Author(s)

L Haim (External organisation)

D. Choukroun (TU Delft - Space Systems Egineering)

Research Group
Space Systems Egineering
DOI related publication
https://doi.org/http://arc.aiaa.org/doi/pdf/10.2514/6.2012-4557
More Info
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Publication Year
2012
Language
English
Research Group
Space Systems Egineering
Pages (from-to)
1-20
ISBN (print)
9781600869389

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