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Abstrakty
The focus of this paper is the design of a selfmaintenance orbit using two natural forces against each other. The effect of perturbations due to Earth’s oblateness up to the third order on both the semi-major axis and eccentricity for a low Earth orbit satellite together with the perturbation due to air drag on the same orbital parameters were used, in order to create self-maintenance orbits. Numerical results were simulated for a low earth orbit satellite,which substantiates the applicability of the results.
Czasopismo
Rocznik
Tom
Strony
56--60
Opis fizyczny
Bibliogr. 9 poz.
Twórcy
autor
- Mathematics Department, College of Sciences and Arts, Qassim University, AlRass, Saudi Arabia; Theoretical Physics Dept., National Research Centre, Dokki, Giza, Egypt
Bibliografia
- [1] King-Hele D. G., Walker D. M. C.: An Irregularity in the Atmospheric Drag Effects on Sputniks 2 and 3, Nature, 182, 860, 1958.
- [2] Sehnal L.: The motion of a close earth satellite, Advances in space Research, 6(9), 151, 1986.
- [3] Kozai Y.: The motion of a close earth satellite, Astronomical Journal, 64, 367, 1959.
- [4] Khalil Kh.: The drag exerted by an oblate rotating atmosphere on an artificial satellite, Applied Mathematics and Mechanics, 23(9),1016, 2002.
- [5] Bezdek, A: Semi analytic Theory of Motion for LEO Satellites Under Air Drag, Planetary and Space Science, 52(14),1233, 2004.
- [6] Ammar M.K, El-Shaboury S.M., Amin M.R.: Third order secular perturbation in the motion of a satellite of a non-spherical planet, Astrophysics and Space Sciences, 340(1),43, 2012.
- [7] Yin ka Fan, S. Y.Ma, Li Jing, Zhou Yun-Liang, Feng Ding-Hua,Wang Xi-Jing: Simulation of orbit decay for LEO satellites caused by atmospheric drag, Chinese Journal of Geophysics, 56(12), 3980, 2013.
- [8] Masoud A., Rahoma W. A., Khattab E. H., Ahmed F.: Construction of Frozen Orbits Using Continuous Thrust Control Theories Considering Earth Oblateness and Solar Radiation Pressure Perturbations, Journal of the Astronautical Sciences, 65(2), 448, 2018.
- [9] Roy A.E.: Orbital Motion, 4thedi., IOP Publishing Ltd, 2005.
Uwagi
Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2021).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-fd81568c-b97f-4026-9e4e-2e53a93c4c22