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Fawzy Ahmed Abd El-Salam
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2010 – 2019
- 2013
- [j12]Fawzy Ahmed Abd El-Salam:
Some New Locally Optimal Control Laws for Sailcraft Dynamics in Heliocentric Orbits. J. Appl. Math. 2013: 353056:1-353056:16 (2013) - 2012
- [j11]Sobhy E. Abd El-Bar
, Fawzy Ahmed Abd El-Salam:
Analytical and Semi-Analytical Treatment of the Satellite Motion in a Resisting Medium. J. Appl. Math. 2012: 489849:1-489849:18 (2012) - 2011
- [j10]Fawzy Ahmed Abd El-Salam:
Air Drag Effects on the Missile Trajectories. J. Appl. Math. 2011: 871304:1-871304:19 (2011)
2000 – 2009
- 2007
- [j9]Yehia A. Abdel-Aziz
An efficient algorithm for orbital evolution of artificial satellite. Appl. Math. Comput. 191(2): 415-428 (2007) - 2006
- [j8]Ahmed A. El-Enna, M. K. Ahmed, Fawzy Ahmed Abd El-Salam:
Analytical treatment of the relativistic and solar radiation pressure effects on an artificial satellite. Appl. Math. Comput. 175(2): 1525-1542 (2006) - [j7]Fawzy Ahmed Abd El-Salam, I. A. El-Tohamy, M. K. Ahmed, Walid Ali Rahoma, M. A. Rassem:
Invariant relative orbits for satellite constellations: A second order theory. Appl. Math. Comput. 181(1): 6-20 (2006) - 2005
- [j6]Fawzy Ahmed Abd El-Salam, M. K. Ahmed
The post-Newtonian effects in the critical inclination problem in artificial satellite theory. Appl. Math. Comput. 161(3): 813-823 (2005) - [j5]Fawzy Ahmed Abd El-Salam, M. K. Ahmed
Canonical solution of the critical inclination problem taking into account PN-corrections. Appl. Math. Comput. 161(3): 825-841 (2005) - [j4]Fawzy Ahmed Abd El-Salam, L. Sehnal:
The effects of the terrestrial infrared radiation pressure on the earth's artificial satellite dynamics. Appl. Math. Comput. 162(3): 1431-1451 (2005) - [j3]Mohamad Radwan
The problem of close approach of two small masses in the field of massive oblate primary. Appl. Math. Comput. 168(1): 389-397 (2005) - [j2]Fawzy Ahmed Abd El-Salam:
Optimization out-of-orbit plane changes using aeroassisted maneuvers. Appl. Math. Comput. 170(2): 1303-1313 (2005) - [j1]Fawzy Ahmed Abd El-Salam, L. Sehnal:
Analytical second-order drag theory with application for lifetime determination of artificial satellites in low earth orbits. Appl. Math. Comput. 171(2): 948-971 (2005)
Coauthor Index
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