NANOSATELLITE MOTION SIMULATION FOR TESTING THE SUN SENSOR

Авторы

  • Yerkebulan Nurgizat Computer Lab of Paris 6 (LIP ), Sorbonne University
  • Alan Dias Rizo Computer Lab of Paris 6 (LIP ), Sorbonne University

DOI:

https://doi.org/10.52167/1609-1817-2021-118-3-34-42

Ключевые слова:

Nanosatellite, solar sensors, vector

Аннотация

Nanosatellite (NS) began to perform complex missions that require high orientation. In this research, we developed a mathematical model of solar sensors to determine the orientation of a NS. Various moments of obtaining the angle of the sun's rays when they hit the solar sensors were presented. The test results of the solar sensors used to simulate various orbit scenarios are described in detail, and graphs of the solar sensor readings are plotted based on the results obtained.

The article deals with modeling the motion of a NS in orbit. The NS is equipped with 6 solar panels. The VTS software was used to simulate the motion of the NS. Also, in the study of determining the orientation, two different problems were considered, that is, when the satellite is in the shadow part of the earth and when it is in the solar part of the earth. For these tasks, a mathematical model for determining the orientation was built. This method is very relevant for the study of small spacecraft.

Биографии авторов

Yerkebulan Nurgizat, Computer Lab of Paris 6 (LIP ), Sorbonne University

Paris, France,  e.nurgizat@mail.ru

Alan Dias Rizo , Computer Lab of Paris 6 (LIP ), Sorbonne University

doctoral student, Lip6, Sorbonne University

Библиографические ссылки

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[9] Hyung-Chul Lim, Hyo-Choong Bang, and Sang-Jong Lee. Adaptive Backstepping Control for Satellite Formation Flying With Mass Uncertainty. Journal of Astronomy and Space Sciences, 23(4):405{414, 2006.

[10]. Rodionov S.A. Osnovy optiki. Konspekt lekcij. –SPb: SPb GITMO (TU), 2000. -167s.

[11] VTS 3.5 User Manual (VTS-MU-G-69-SPB-7.3)

[12] CelesTrak: Current NORAD Two-Line Element Sets. Available at https://www.celestrak.com/NORAD/elements/, (Accessed on 08/04/2021).

[13] Filho, Edemar Morsch, Seman, Laio Oriel, Rigo, Cezar Antônio, Nicolau, Vicente de Paulo, Ovejero, Raúl García, Leithardt, Valderi Reis Quietinho, 2020, Energies, Irradiation Flux Modelling for Thermal–Electrical Simulation of CubeSats: Orbit, Attitude and Radiation Integration doi:10.3390/en13246691 https://www.mdpi.com/1996-1073/13/24/6691.

Загрузки

Опубликован

17.09.2021

Как цитировать

Nurgizat, Y., & Dias Rizo , A. (2021). NANOSATELLITE MOTION SIMULATION FOR TESTING THE SUN SENSOR. Вестник КазАТК, 118(3), 34–42. https://doi.org/10.52167/1609-1817-2021-118-3-34-42

Выпуск

Раздел

Автоматика, телемеханика, связь, электроэнергетика, информационные системы