| Visibility intervals between two artificial satellites under the action of Earth oblateness MHMH M. K. Ammar, M. R. Amin Applied Mathematics and Nonlinear Sciences 3 (2), 353-374, 2018 | 23 | 2018 |
| Calculation of line of site periods between two artificial satellites under the action air drag MHMH M. K. Ammar, M. R. Amin Applied Mathematics and Nonlinear Sciences 3 (2), 339-352, 2018 | 17 | 2018 |
| Third-order secular solution of the variational equations of motion of a satellite in orbit around a non-spherical planet MK Ammar, SM El Shaboury, MR Amin Astrophysics and Space Science 340, 43-61, 2012 | 14 | 2012 |
| THE EFFECT OF SOLAR RADIATION PRESSURE AND PLANET OBLATENESS ON THE LOCATION AND STABILITY OF LAGRANGIAN POINTS IN SOLAR SYSTEM PLANETS MR AMIN Fractals 30 (10), 10, 2022 | | 2022 |
| Self-Maintenance Orbits Using The perturbations Due to Air Drag and Due to Earth’s Oblateness MR Amin Mechanics and Mechanical Engineering 24 (1), 56-60, 2020 | | 2020 |
| Optimal Generalized Hohmann Transfer with Plane Change Using Lagrange Multipliers. OM Kamel, AS Soliman Mechanics & Mechanical Engineering 21 (1), 2017 | | 2017 |
| The Stability of the Triangular Points of the Restricted three Body Problem when both the Primaries are Triaxial Rigid Bodies SM Elshaboury, MR Amin Scholars Journal of Physics, Mathematics and Statistics 2 (2B), 269-275, 2015 | | 2015 |
| VISIBILITY INTERVALS BETWEEN TWO SATELLITES ORBITS UNDER J2 -GRAVITY AND DRAG FORCE m.r.amin W.N.Ahmed ,M.E.Awad ,I.A.Hassan , M.K.Ammar Al Azhar Buletin of Science 26 (2), 1-10, 2015 | | 2015 |
| Elliptic Restricted Three Body Problems Under The Effect of Solar Radiation Pressure M. K. Ammar, M. R. Amin Buletin of Faculty of Science, Cairo University 72, 37-52, 2004 | | 2004 |
Mohamed HassanInstructor of Applied Mathematics - Department of Mathematics - College of Science - HelwanVerified email at science.helwan.edu.eg
