| 2007 |
|---|
| 9 | EE | Yehia A. Abdel-Aziz,
F. A. Abd El-Salam:
An efficient algorithm for orbital evolution of artificial satellite.
Applied Mathematics and Computation 191(2): 415-428 (2007) |
| 2006 |
|---|
| 8 | EE | Ahmed A. El-Enna,
M. K. Ahmed,
F. A. Abd El-Salam:
Analytical treatment of the relativistic and solar radiation pressure effects on an artificial satellite.
Applied Mathematics and Computation 175(2): 1525-1542 (2006) |
| 7 | EE | F. A. Abd El-Salam,
I. A. El-Tohamy,
M. K. Ahmed,
W. A. Rahoma,
M. A. Rassem:
Invariant relative orbits for satellite constellations: A second order theory.
Applied Mathematics and Computation 181(1): 6-20 (2006) |
| 2005 |
|---|
| 6 | EE | F. A. Abd El-Salam,
M. K. Ahmed,
Mohamad Radwan:
The post-Newtonian effects in the critical inclination problem in artificial satellite theory.
Applied Mathematics and Computation 161(3): 813-823 (2005) |
| 5 | EE | F. A. Abd El-Salam,
M. K. Ahmed:
Canonical solution of the critical inclination problem taking into account PN-corrections.
Applied Mathematics and Computation 161(3): 825-841 (2005) |
| 4 | EE | F. A. Abd El-Salam,
L. Sehnal:
The effects of the terrestrial infrared radiation pressure on the earth's artificial satellite dynamics.
Applied Mathematics and Computation 162(3): 1431-1451 (2005) |
| 3 | EE | Mohamad Radwan,
M. K. Ahmed,
F. A. Abd El-Salam:
The problem of close approach of two small masses in the field of massive oblate primary.
Applied Mathematics and Computation 168(1): 389-397 (2005) |
| 2 | EE | F. A. Abd El-Salam:
Optimization out-of-orbit plane changes using aeroassisted maneuvers.
Applied Mathematics and Computation 170(2): 1303-1313 (2005) |
| 1 | EE | F. A. Abd El-Salam,
L. Sehnal:
Analytical second-order drag theory with application for lifetime determination of artificial satellites in low earth orbits.
Applied Mathematics and Computation 171(2): 948-971 (2005) |
