Zobrazeno 1 - 8
of 8
pro vyhledávání: '"M. K. Ammar"'
Publikováno v:
Applied Mathematics and Nonlinear Sciences. 3:339-352
In a previous (herein referred to as Ammar, Amin and Hassan Paper [1]) the statement of the problem was formulated and the basic visibility function between two satellites in terms of the orbital elements and time were derived. In this paper the pert
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0de879a3815b4ef83cd69de0283340e2
https://doi.org/10.21042/amns.2018.2.00027
https://doi.org/10.21042/amns.2018.2.00027
Publikováno v:
Applied Mathematics and Nonlinear Sciences. 3:353-374
This paper presents an analytical method to determine the rise-set times of satellite-satellite visibility periods in different orbits. The Visibility function in terms of the orbital elements of the two satellites versus the time were derived explic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cd4e14ca8677dedabcf3649eff8ffd06
https://doi.org/10.21042/amns.2018.2.00028
https://doi.org/10.21042/amns.2018.2.00028
Publikováno v:
Applied Mathematics and Nonlinear Sciences. 2:259-270
This paper is concerned on the distribution of a homogeneous isotropic elastic medium with diffusion under the effect of Three-phase-lag model. Normal mode analysis is used to express the exact expressions for temperature, displacements and stresses
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6e8536bac80dc3d50d951f0011c6891f
https://doi.org/10.21042/amns.2017.1.00022
https://doi.org/10.21042/amns.2017.1.00022
Publikováno v:
Al-Azhar Bulletin of Science. 26:1-10
The research introduces a general analytical and computational technique for satellite-to-satellite visibility. The effect of earth’s oblateness and drag force were taken into account.The Visibility function in terms of the orbital elements of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5a415f0021c7dbf1a61b1b831159e0be
https://doi.org/10.21608/absb.2015.22634
https://doi.org/10.21608/absb.2015.22634
Autor:
M. K. Ammar
Publikováno v:
Astrophysics and Space Science. 313:393-408
In this paper the effect of solar radiation pressure on the location and stability of the five Lagrangian points is studied, within the frame of elliptic restricted three-body problem, where the primaries are the Sun and Jupiter acting on a particle
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5c0e8c3873b40e35c9acc67aadb95fce
https://doi.org/10.1007/s10509-007-9709-z
https://doi.org/10.1007/s10509-007-9709-z
Autor:
M. K. Ammar
Publikováno v:
Astrophysics and Space Science. 312:17-22
In a previous paper (Ammar in Proc. Math. Phys. 77:99, 2002) the statement of the problem was formulated and the basic equations of motion were formed in terms of variables suitable for the applications in the problem of asteroid motion close to 2:1
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4850ee32e87654821432c10d1106288b
https://doi.org/10.1007/s10509-007-9603-8
https://doi.org/10.1007/s10509-007-9603-8
Autor:
Osman M. Kamel, M. K. Ammar
Publikováno v:
Acta Astronautica. 59:1111-1116
Firstly we derive Gauss’ perturbation equation for parabolic motion using Murray–Dermott and Kovalevsky procedures. Secondly, we easily deduce the variations of the orbital elements for the parabolic trajectories due to a small impulse at any poi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a7e094546c4573d81a47dcf7ec6c87ce
https://doi.org/10.1016/j.actaastro.2006.03.008
https://doi.org/10.1016/j.actaastro.2006.03.008
Autor:
M. K. Ammar, Osman M. Kamel
Publikováno v:
Acta Astronautica. 58:243-250
We shall investigate the problem of the differential corrections of the orbital elements a , e of the final elliptic orbit, in order that we might obtain the required very precise one. This will be achieved by the application of differential motor th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0474527622f7708c8f72b18d7d92c8a5
https://doi.org/10.1016/j.actaastro.2005.09.010
https://doi.org/10.1016/j.actaastro.2005.09.010