F. A. Abd El-Salam - researchr alias

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2025

Semi-analytical computation of commensurate semimajor axes of resonant orbits including second-order gravitational perturbationsZ. A. Mabrouk, F. A. Abd El-Salam, A. Owis, Wesam Elmahy. ascom, 51:100940, 2025. [doi]

2007

An efficient algorithm for orbital evolution of artificial satelliteYehia A. Abdel-Aziz, F. A. Abd El-Salam. amc, 191(2):415-428, 2007. [doi]

2006

Analytical treatment of the relativistic and solar radiation pressure effects on an artificial satelliteAhmed A. El-Enna, M. K. Ahmed, F. A. Abd El-Salam. amc, 175(2):1525-1542, 2006. [doi]

Invariant relative orbits for satellite constellations: A second order theoryF. A. Abd El-Salam, I. A. El-Tohamy, M. K. Ahmed, W. A. Rahoma, M. A. Rassem. amc, 181(1):6-20, 2006. [doi]

2005

Canonical solution of the critical inclination problem taking into account PN-correctionsF. A. Abd El-Salam, M. K. Ahmed. amc, 161(3):825-841, 2005. [doi]

The post-Newtonian effects in the critical inclination problem in artificial satellite theoryF. A. Abd El-Salam, M. K. Ahmed, Mohamad Radwan. amc, 161(3):813-823, 2005. [doi]

The effects of the terrestrial infrared radiation pressure on the earth s artificial satellite dynamicsF. A. Abd El-Salam, L. Sehnal. amc, 162(3):1431-1451, 2005. [doi]

Optimization out-of-orbit plane changes using aeroassisted maneuversF. A. Abd El-Salam. amc, 170(2):1303-1313, 2005. [doi]

Analytical second-order drag theory with application for lifetime determination of artificial satellites in low earth orbitsF. A. Abd El-Salam, L. Sehnal. amc, 171(2):948-971, 2005. [doi]

The problem of close approach of two small masses in the field of massive oblate primaryMohamad Radwan, M. K. Ahmed, F. A. Abd El-Salam. amc, 168(1):389-397, 2005. [doi]

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