Fawzy Ahmed Abd El-Salam

According to our database, Fawzy Ahmed Abd El-Salam authored at least 12 papers between 2005 and 2013.

Collaborative distances:

• Dijkstra number of seven.
• Erdős number of six.

2013

Some New Locally Optimal Control Laws for Sailcraft Dynamics in Heliocentric Orbits.

Fawzy Ahmed Abd El-Salam

J. Appl. Math., 2013

2012

Analytical and Semi-Analytical Treatment of the Satellite Motion in a Resisting Medium.

Sobhy E. Abd El-Bar, Fawzy Ahmed Abd El-Salam

J. Appl. Math., 2012

2011

Air Drag Effects on the Missile Trajectories.

Fawzy Ahmed Abd El-Salam

J. Appl. Math., 2011

2007

An efficient algorithm for orbital evolution of artificial satellite.

Yehia A. Abdel-Aziz, Fawzy Ahmed Abd El-Salam

Appl. Math. Comput., 2007

2006

Invariant relative orbits for satellite constellations: A second order theory.

Fawzy Ahmed Abd El-Salam, I. A. El-Tohamy, M. K. Ahmed, Walid Ali Rahoma, M. A. Rassem

Appl. Math. Comput., 2006

Analytical treatment of the relativistic and solar radiation pressure effects on an artificial satellite.

Ahmed A. El-Enna, M. K. Ahmed, Fawzy Ahmed Abd El-Salam

Appl. Math. Comput., 2006

2005

The problem of close approach of two small masses in the field of massive oblate primary.

Mohamad Radwan, M. K. Ahmed, Fawzy Ahmed Abd El-Salam

Appl. Math. Comput., 2005

The effects of the terrestrial infrared radiation pressure on the earth's artificial satellite dynamics.

Fawzy Ahmed Abd El-Salam, L. Sehnal

Appl. Math. Comput., 2005

Analytical second-order drag theory with application for lifetime determination of artificial satellites in low earth orbits.

Fawzy Ahmed Abd El-Salam, L. Sehnal

Appl. Math. Comput., 2005

The post-Newtonian effects in the critical inclination problem in artificial satellite theory.

Fawzy Ahmed Abd El-Salam, M. K. Ahmed, Mohamad Radwan

Appl. Math. Comput., 2005

Canonical solution of the critical inclination problem taking into account PN-corrections.

Fawzy Ahmed Abd El-Salam, M. K. Ahmed

Appl. Math. Comput., 2005

Optimization out-of-orbit plane changes using aeroassisted maneuvers.

Fawzy Ahmed Abd El-Salam

Appl. Math. Comput., 2005