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Concurrent rendezvous control of underactuated spacecraft
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology.
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology.
2017 (English)In: Acta Astronautica, ISSN 0094-5765, E-ISSN 1879-2030, Vol. 138, 28-42 p.Article in journal (Refereed) Published
Abstract [en]

The concurrent control of spacecraft equipped with one-axis unilateral thruster and three-axis attitude actuator is considered in this paper. The proposed control law utilizes attitude control channels along with the single thrust force concurrently, for three-dimensional trajectory tracking and rendezvous with a target object. The concurrent controller also achieves orbital transfer to low Earth orbits with long range separation. To demonstrate the orbit transfer capabilities of the concurrent controller, a smooth elliptical orbit transfer trajectory for co-planar circular orbits is designed. The velocity change and energy consumption of the designed orbit transfer trajectory is observed to be equivalent to that of Hohmann transfer.

Place, publisher, year, edition, pages
Elsevier, 2017. Vol. 138, 28-42 p.
National Category
Other Electrical Engineering, Electronic Engineering, Information Engineering
Research subject
Onboard space systems
Identifiers
URN: urn:nbn:se:ltu:diva-63471DOI: 10.1016/j.actaastro.2017.05.003Scopus ID: 2-s2.0-85019892967OAI: oai:DiVA.org:ltu-63471DiVA: diva2:1097057
Note

Validerad;2017;Nivå 2;2017-06-02 (andbra)

Available from: 2017-05-22 Created: 2017-05-22 Last updated: 2017-07-07Bibliographically approved

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Citation style
  • apa
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Output format
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  • asciidoc
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