Influence of geomagnetic field models on analytical propagator for SPIN stabilized satellites / Influência de modelos de campo geomagnético em analíticos propagador de satélites estabilizados com SPIN

Authors

  • Maria Cecília Zanardi Brazilian Journals Publicações de Periódicos, São José dos Pinhais, Paraná
  • Victor Mota

DOI:

https://doi.org/10.34117/bjdv6n3-442

Keywords:

Analytical Propagators, Artificial Satellites, Environmental Torques, Satellite Attitude.

Abstract

 This work explores the impacts of using dipole or quadrupole models for Earth’s magnetic field when an analytical propagator calculates residual and eddy current torques on spin-stabilized satellites. Comprising the gravity gradient, solar radiation pressure, aerodynamic, and the aforementioned torques, the propagators used data from Brazilian satellites SCD1 and SCD2, provided by the National Institute for Space Research (INPE). Ranging about two decades in total, the selected simulation periods had their respective initial data propagated by both programs and then compared with actual data from the satellites, both updating the simulation with new daily data and not. The first propagator, called GSAM, which uses the dipole model to calculate the magnetic torques, was used to screen for simulation periods due to its swift running time. The second propagator uses the quadrupole model and is called GSAMQ. The mean deviations for the spin velocity, right ascension and declination angles were compared for both satellites, which showed that the programs better predict the spatial orientation of satellite SCD2 over SCD1, especially GSAMQ. It is also demonstrated that the programs’ precision heavily relies on the initial data, suggesting that a statistical approach of GSAMQ’s performance could shed more light on its accuracy.

Analytical Propagators, Artificial Satellites, Environmental Torques, Satellite Attitude.

References

Garcia, R.V., 2007. Satélites Estabilizados por Rotação e o Torque Magnético Residual. Tese de Mestrado, Universidade Estadual Paulista, Guaratinguetá, Brasil.

Kuga, H.K., Ferreira, L.D. e Guedes, U.T., 1987. “Simulação de atitude e de manobras para o satélite brasileiro estabilizado por rotação”. Relatório Técnico, INPE-4271-PRE/1143.

Mota, V. e Zanardi, M.C., 2018. “Validação do propagador de atitude gsam de satélites estabilizados por rotação para diferentes períodos de simulação”. Proceeding Series of the Brazilian Society of Computational and Applied Mathematics, Vol. 6, No. 1.

Motta, G.B., 2014. Predição Analítica do Movimento Rotacional de Satélites Estabilizados. Tese de Mestrado, Universidade Estadual Paulista, Guaratinguetá, Brasil.

Wertz, J.R., 1978. Spacecraft Attitude Determination and Control. Springer Science and Business Media, London, UK.

Zanardi, M.C., Celestino, C.C., Motta, G.B., França, E.M. e Garcia, R.V., 2018. “Analysis of analytical attitude propagators for spin stabilized satellites”. Computational and Applied Mathematics, Vol. 37, pp. 96–109.

Zanardi, M.C., Orlando, V., Motta, G.B., Pelosi, T. e Silva, W.R., 2016. “Numerical and analytical approach for the spin-stabilized satellite attitude propagation”. Computational and Applied Mathematics, Vol. 1, pp. 1–13.

Downloads

Published

2020-03-27

How to Cite

Zanardi, M. C., & Mota, V. (2020). Influence of geomagnetic field models on analytical propagator for SPIN stabilized satellites / Influência de modelos de campo geomagnético em analíticos propagador de satélites estabilizados com SPIN. Brazilian Journal of Development, 6(3), 15648–15663. https://doi.org/10.34117/bjdv6n3-442

Issue

Section

Original Papers