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

L Haim; D Choukroun

doi:http://arc.aiaa.org/doi/pdf/10.2514/6.2012-4557

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

L Haim, D Choukroun

Space Systems Engineering

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

Original language	English
Title of host publication	Proceeings of the AIAA Guidance, Navigation, and Control Conference, AIAA 2012-4557
Editors	s.n.
Place of Publication	Minneapolis, MN
Publisher	American Institute of Aeronautics and Astronautics Inc. (AIAA)
Pages	1-20
Number of pages	20
ISBN (Print)	9781600869389
DOIs	https://doi.org/http://arc.aiaa.org/doi/pdf/10.2514/6.2012-4557
Publication status	Published - 2012
Event	AIAA Guidance, Navigation, and Control Cohference 2012, Minneaplois, MN, USA - Minneapolis, MN Duration: 13 Aug 2012 → 16 Aug 2012

Publication series

Name
Publisher	AIAA

Conference

Conference	AIAA Guidance, Navigation, and Control Cohference 2012, Minneaplois, MN, USA
Period	13/08/12 → 16/08/12

Keywords

Conf.proc. > 3 pag

Access to Document

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-4557

Cite this

Haim, L., & Choukroun, D. (2012). Optimized state-dependent Riccati Equation method for spacecraft attitude estimation and control. In s.n. (Ed.), Proceeings of the AIAA Guidance, Navigation, and Control Conference, AIAA 2012-4557 (pp. 1-20). American Institute of Aeronautics and Astronautics Inc. (AIAA). https://doi.org/http://arc.aiaa.org/doi/pdf/10.2514/6.2012-4557

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title = "Optimized state-dependent Riccati Equation method for spacecraft attitude estimation and control",

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publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

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note = "AIAA Guidance, Navigation, and Control Cohference 2012, Minneaplois, MN, USA ; Conference date: 13-08-2012 Through 16-08-2012",

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Haim, L & Choukroun, D 2012, Optimized state-dependent Riccati Equation method for spacecraft attitude estimation and control. in s.n. (ed.), Proceeings of the AIAA Guidance, Navigation, and Control Conference, AIAA 2012-4557. American Institute of Aeronautics and Astronautics Inc. (AIAA), Minneapolis, MN, pp. 1-20, AIAA Guidance, Navigation, and Control Cohference 2012, Minneaplois, MN, USA, 13/08/12. https://doi.org/http://arc.aiaa.org/doi/pdf/10.2514/6.2012-4557

Optimized state-dependent Riccati Equation method for spacecraft attitude estimation and control. / Haim, L; Choukroun, D.
Proceeings of the AIAA Guidance, Navigation, and Control Conference, AIAA 2012-4557. ed. / s.n. Minneapolis, MN: American Institute of Aeronautics and Astronautics Inc. (AIAA), 2012. p. 1-20.

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

TY - GEN

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