Laser orbital perturbations in Hamiltonian framework

  • Authors

    • M. I El-Saftawy King Abdul-Aziz University, Faculty of Science, Department of Astronomical Science, Jeddah, K.S.A , Sun and Space researches lab, National Institute of Astronomy and Geophysics (NRIAG), Helwan Egypt.
    • Nabawia Khalifa Department of Basic Science, Deanship of Preparatory Year, University of Hail, Hail, KSA, Sun and Space researches lab, National Institute of Astronomy and Geophysics (NRIAG), Helwan Egypt.
    2018-04-30
    https://doi.org/10.14419/ijaa.v6i1.9786
  • Canonical Formulation, Laser Radiation Pressure and Orbital Perturbations.

  • Abstract

    The effect of laser photon pressure on the spacecraft’s orbit is modeled. The force model developed taking into consideration atmospheric beam attenuation. However, adaptive optics assumed fixed on the laser system in order to eliminate the effect of atmospheric turbulence. The force of a single laser pulse proved as a conservative force. Consequently, its potential obtained using Legender polynomial. Assuming a spherical Earth, the Hamiltonian of the problem developed in terms of Dalaunay elements up to the first zonal harmonic. Using different ground-based laser systems, the model applied to the satellite Ajisai of NORAD ID 16908 and the LEO debris ASTRO-F DEB of NORD ID 29054. The numerical results emphasized that laser pressure has an effect on the orbit and it is well agreed with the results of the Newtonian treatment of the problem.

  • References

    1. [1] Jonathan W. Campbell (2000) Using Lasers in Space: Laser Orbital Debris Removal and Asteroid Deflection. Occasional Paper No. 20 Center for Strategy and Technology Air War College.

      [2] El-Saftawy M.I., and Makram Ibrahim (2004) "The laser shots as a perturbing force on spacecraft's orbit", NRIAG J. of Astronomy and Astrophysics, Special issue.

      [3] El-Saftawy M.I. (2006) Orbital perturbation due to laser pressure in absence of Earth's atmosphere ", NRIAG J. of Astronomy and Astrophysics, special issue.

      [4] El-Saftawy M.I. and Nabawia S. Khalif (2008) Artificial Radiation Effect on Spacecraft's Orbit considering atmospheric beam attenuation. First Middle East and Africa IAU-Regional Meeting Proceedings MEARIM No. 1.

      [5] Nabawia S. khalifa (2009) Effect of an Artificial Radiant Force on the Spacecraft's Orbit. PhD. Thesis, Cairo University.

      [6] James Mason, Jan Stupl, William Marshall and Creon Levit (2011) Orbital Debris-Debris Collision Avoidance. Journal of Advances in Space Research, vol. 48. https://doi.org/10.1016/j.asr.2011.08.005.

      [7] El-Saftawy M. I., Afaf M. Abd El-Hameed, and Nabawia S. Khalifa (2007) Analytical Studies of Laser Beam Propagation through the Atmosphere. Proceeding of 6th International Conference on Laser Science and Applications (ICLAS-07), Cairo, Egypt.

      [8] Danielson E., Levin J., Abrams E. (2003) Meteorology second edition, McGraw-Hill Companies.

      [9] Prilutsky O.F. and Fomenkova M.N. (1990) Appendix laser beam scattering in the atmosphere. Science & Global Security, Vol. 2. https://doi.org/10.1080/08929889008426349.

      [10] Escobal P.R. (1965) Methods of Orbit Determination. John Wiley and Sons, Inc., New York, London, Sydney.

      [11] Sasaki, M and Hashimoto H. (1987) Launch and Observation of the Experimental Geodetic Satellite of Japan. IEEE Transactions on Geoscience and Remote Sensing, Volume 25, No. 5. https://doi.org/10.1109/TGRS.1987.289830.

      [12] Milani, A., Nobili, A.M. and Farinella, P. (1987) non-gravitational perturbations and satellite geodesy, IOP Publishing Ltd.

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  • How to Cite

    El-Saftawy, M. I., & Khalifa, N. (2018). Laser orbital perturbations in Hamiltonian framework. International Journal of Advanced Astronomy, 6(1), 12-16. https://doi.org/10.14419/ijaa.v6i1.9786

    Received date: 2018-03-01

    Accepted date: 2018-03-29

    Published date: 2018-04-30