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Quaternion-based attitude control design and hardware-in-the-loop simulation of suborbital modules with cold gas thrusters
Department of Aerospace Engineering, K.N.T University of Technology, Tehran, Iran.
Department of Aerospace Engineering, K.N.T University of Technology, Tehran, Iran.
Institute for Aerospace Studies, University of Toronto, Toronto, Canada.ORCID iD: 0000-0003-4977-6339
2015 (English)In: Journal of Aerospace Engineering, ISSN 0893-1321, E-ISSN 1943-5525, Vol. 229, no 4, p. 717-735Article in journal (Refereed) Published
Place, publisher, year, edition, pages
2015. Vol. 229, no 4, p. 717-735
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Other Electrical Engineering, Electronic Engineering, Information Engineering
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URN: urn:nbn:se:ltu:diva-4143DOI: 10.1177/0954410014539294ISI: 000350485600011Scopus ID: 2-s2.0-84924912211Local ID: 2089f8a5-02ae-4a7a-a1e2-2151c1326071OAI: oai:DiVA.org:ltu-4143DiVA, id: diva2:977007
Note

Upprättat; 2015; 20150206 (ninhul)

Available from: 2016-09-29 Created: 2016-09-29 Last updated: 2024-08-16Bibliographically approved

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Emami, M Reza

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