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Quaternion-based attitude control design and hardware-in-the-loop simulation of suborbital modules with cold gas thrusters
Institute for Aerospace Studies, University of Toronto.ORCID iD: 0000-0003-4977-6339
Department of Aerospace Engineering, K.N.T University of Technology, Tehran.
Department of Aerospace Engineering, K.N.T University of Technology, Tehran.
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
Abstract [en]

This paper discusses design and implementation of a quaternion-based attitude control system for the short-duration mission of suborbital modules using cold-gas thrusters. The quaternion-based controller generates a command torque for each channel, and a pulse-width pulse-frequency (PWPF) modulator determines the required fire signals for the thrusters. The system performance is examined through both numerical and hardware-in-the-loop simulations.

Place, publisher, year, edition, pages
2015. Vol. 229, no 4, p. 717-735
National Category
Other Electrical Engineering, Electronic Engineering, Information Engineering
Research subject
Onboard space systems
Identifiers
URN: urn:nbn:se:ltu:diva-4143DOI: 10.1177/0954410014539294Local ID: 2089f8a5-02ae-4a7a-a1e2-2151c1326071OAI: oai:DiVA.org:ltu-4143DiVA, id: diva2:977007
Note
Uppr├Ąttat; 2015; 20150206 (ninhul)Available from: 2016-09-29 Created: 2016-09-29 Last updated: 2017-12-15Bibliographically approved

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