Study and selection of coil pa rameters for NTUU«KPI» microsatellite

Authors

  • Валерій Петрович Зінченко National technical university of Ukraine “Kyiv polytechnic institute” 37, Prospect Peremohy, 03056, Kyiv-56, Ukraine, Ukraine https://orcid.org/0000-0001-8745-3325
  • Ганна Володимирівна Сарибога National technical university of Ukraine “Kyiv polytechnic institute” 37, Prospect Peremohy, 03056, Kyiv-56, Ukraine, Ukraine https://orcid.org/0000-0001-8745-3325

DOI:

https://doi.org/10.15587/2312-8372.2014.25336

Keywords:

moment of rotation, magnetic coils, current, magnetic devices, microsatellite

Abstract

Microsatellite motion relative to the center of mass (rotational motion) is much more sensitive to external perturbations than the motion of the center of mass along the trajectory, which does not notice them at all. That is why angular motion control of the microsatellite, or, in other words, control systems relative to the center of mass, is as a rule the most difficult and crucial part of the onboard equipment. The efficiency of the MS and, consequently, efficiency of practical tasks they perform significantly depends on the functionality of these systems, as well as their technical and operating characteristics. Performance of the «KPI» microsatellite when using the system control unit — magnetic coils for space orientation of microsatellites is defined. For the microsatellite to have the correct orientation, it is necessary to select such parameters to be able to manage the current supply in the coils proportionally to the required rotation in space. The research data and results obtained are used in designing on board systems of spacecrafts.

Author Biographies

Валерій Петрович Зінченко, National technical university of Ukraine “Kyiv polytechnic institute” 37, Prospect Peremohy, 03056, Kyiv-56, Ukraine

Candidate of Technical Sciences, Associate Professor

Department of  Experimental Research Automation

Ганна Володимирівна Сарибога, National technical university of Ukraine “Kyiv polytechnic institute” 37, Prospect Peremohy, 03056, Kyiv-56, Ukraine

Senior teacher

Department of Aircraft Control Devices and Systems

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Published

2014-06-24

How to Cite

Зінченко, В. П., & Сарибога, Г. В. (2014). Study and selection of coil pa rameters for NTUU«KPI» microsatellite. Technology Audit and Production Reserves, 3(4(17), 58–64. https://doi.org/10.15587/2312-8372.2014.25336

Issue

Vol. 3 No. 4(17) (2014): Production reserves

Section

Production reserves

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Copyright (c) 2016 Валерій Петрович Зінченко, Ганна Володимирівна Сарибога

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