بررسی مدار انتقال LEO به GEO با استفاده از نقاط لاگرانژی سیستم زمین- خورشید در حضور اغتشاشات

1. SabooriDarabi, E., Zardashti, R., Kordjazi, H., Esmaeli, M.: “Stability of Lagrangian Points in Sun-Earth system & RTBP”, April, 2016(in Persian).##
2. Koon, Wang sang, Martin, W.Lo, Marsden, Jerrold E.: “Dynamical Systems, the Three Body Problem and Space Mission Design”, 2006.##
3. Esther Barrabes, Laura Garcia-Taberner, and Gerard Gomez: A note on transfer from LEOs to GEOs visiting libration points of Sun-Earth CRTBP, Advances in Space Research, Vol 57, pp. 938-947, 2016.##
4. Herrera, E., 2008. “Study of LEO to GEO transfers via L₁ the Sun–Earth or Earth–Moon libration points (Master’s thesis)”, UPC.##
5. Curtis, H.D.: “Orbital Mechanics for Engineering Students” 3^thed, New York:McGraw-Hill, 2010.##
6. Battin, Richard H.: “An Introduction to the Mathematics and Methods of Astrodynamics”, AIAA education series, 2001.##
7. Gomez,G., Llibre,J., Martinez,R., Simo,C.: “Dynamics and Mission Design Near Libration Points-Vol. I Fundamentals: The Case of Collinear Libration Points”, World Scientific Publishing, 2001.##
8. Adnan, M.SK,Razali, R., Azlin, and Md. & Said, Md.: “Study of Perturbation Effect on Satellite Orbit Using Cowell’s Method”, School of Aerospace Engineering, 2013.##
9. Elenna, AA: “Analytical Treatment of the Earth Oblateness & Solar Radiation Pressure Effects on an Artificial Satellite I. the Equations of Motion”, Mathematics & Computation 138(2003).##

10. Adnan, M.SK. Razali, R., Azlin, Md. & Said, Md.: Study of Perturbation Effect on Satellite Orbit Using Cowell’s Method, School of Aerospace Engineering, 2013.Han-qing ZHANG and Yan-jun LI, ‘’ The Design of Earth-Moon Transfer Trajectory Using Sun-Earth Ll Libration Point Manifolds”, 3rd International Conference on Advanced Computer Control, IEEE, 2011.##