Effectiveness of KS elements in satellite orbit prediction using earth's gravity, drag and solar radiation pressure

  • Authors

    • T. R. Saritha Kumari Vikram Sarabhai Space Centre
    • M. Xavier James Raj Applied Mathematics Division, Vikram Sarabhai Space Centre, Thiruvananthapuram
    2020-07-12
    https://doi.org/10.14419/ijaa.v8i1.28714
  • Orbit Prediction, Solar Radiation Pressure, Semi-Major Axis, KS Elements.

  • Abstract

    Satellite moving under the gravitational field of Earth deviates from its two-body elliptic orbit, due to the combined effects of the gravitational field of Earth, atmospheric drag, solar radiation pressure, third-body gravitational effects, etc. This paper utilizes the KS regular element equations to solve Newtonian equations of motion to obtain numerical solution with respect to perturbing forces, like, Earth's gravity (includes zonal, sectorial and tesseral harmonics terms), atmospheric drag and solar radiation pressure. Effectiveness of the theory is illustrated by comparing the results with some of the existing theories in literature.

     

  • References

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  • How to Cite

    R. Saritha Kumari, T., & Xavier James Raj, M. (2020). Effectiveness of KS elements in satellite orbit prediction using earth’s gravity, drag and solar radiation pressure. International Journal of Advanced Astronomy, 8(1), 19-26. https://doi.org/10.14419/ijaa.v8i1.28714

    Received date: 2019-04-01

    Accepted date: 2019-07-06

    Published date: 2020-07-12