Results 11 to 20 of about 54,135 (313)

Comparison of the coordinates of the major planets, Moon, and Sun obtained based on a new principle of interaction and of the data bank DE405

open access: yesVestnik Samarskogo Gosudarstvennogo Tehničeskogo Universiteta. Seriâ: Fiziko-Matematičeskie Nauki, 2016
In this paper the comparison of orbit coordinates and elements of large planets, the Moon and the Sun obtained on the basis of a new principle of interaction and of data bank DE405 is made.
Anatoly F Zausaev
doaj   +1 more source

Calculation Mars – Earth distance and Mars orbital elements with Julian date

open access: yesIraqi Journal of Physics, 2023
In this paper, the Mars orbital elements were calculated. These orbital elements—the major axis, the inclination (i), the longitude of the ascending node (W), the argument of the perigee (w), and the eccentricity (e)—are essential to knowing the size ...
Atared Y. Qahtan
doaj   +1 more source

Nilpotent Orbits and Commutative Elements

open access: yesJournal of Algebra, 1997
zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Fan, C.Kenneth, Stembridge, John R.
openaire   +2 more sources

Comparative analysis of mathematical models for estimating the impact probability of asteroid Apophis

open access: yesVestnik Samarskogo Gosudarstvennogo Tehničeskogo Universiteta. Seriâ: Fiziko-Matematičeskie Nauki, 2012
Methods for estimating the impact probability of asteroid Apophis were implemented. The probability of a collision was assessed using two methods: the Monte Carlo method, and the second one, utilizing a ratio between the interval of values of orbital ...
Anatoliy F Zausaev, Andrey E Derevyanka
doaj   +3 more sources

Orbital estimation of spacecraft under unknown low-thrust acceleration (Second report: estimation of osculating orbital elements)

open access: yesNihon Kikai Gakkai ronbunshu, 2015
As low-thrust propulsion technology becomes increasingly popular, orbital estimation for low-thrust spacecraft may become an area of increasing interest. More frequent use of low-thrust propulsion to place satellites in orbit gives more opportunities for
Naoki DATE, Mai BANDO, Shinji HOKAMOTO
doaj   +1 more source

New orbital elements for 5 double stars [PDF]

open access: yesSerbian Astronomical Journal, 2001
In this paper are presented recalculated elliptical and Thiel-Innes orbitatal elements for the following double stars: WDS05255-0033, WDS12272+2701, WDS 13336+2944 and WDS 21031+0132 (two versions).
Olević D., Jovanović P.
doaj   +1 more source

Effects Of Direct And Indirect Solar Radiation Pressure In Orbital Parameters Of GPS Satelittes

open access: yesAnalele Stiintifice ale Universitatii Ovidius Constanta: Seria Matematica, 2014
In this paper we determined the variation of the Keplerian orbital elements of a GPS satellite due to the direct and indirect action of solar radiation pressure. For this study, we created a soft program to determine the Keplerian elements.
Lupu Sergiu, Zaharescu Eugen
doaj   +1 more source

Erratum: “On the Orbital Elements of the Two-body Problem with Slowly Decreasing Mass: The Gyldén–Mestchersky Cases” (2020, AJ, 160, 203)

open access: yesThe Astronomical Journal, 2023
In Abad et al., we studied the time evolution of orbital elements in the so-called “Gyldén–Mestchersky cases.” Actually the plots represent the evolution of orbital elements with respect to the eccentric anomaly, related with time through Kepler’s ...
Alberto Abad   +3 more
doaj   +1 more source

Mean Orbital Elements for Geosynchronous Orbit - II - Orbital inclination, longitude of ascending node, mean longitude [PDF]

open access: yesJournal of Astronomy and Space Sciences, 1990
The osculating orbital elements include the mean, secular, long period, and short period terms. The iterative algorithm used for conversion of osculating orbital elements to mean orbital elements is described.
Kyu-Hong Choi   +3 more
doaj  

Comparison of various mathematical models on the example of solving the equations of the movement of large planets and the Moon

open access: yesVestnik Samarskogo Gosudarstvennogo Tehničeskogo Universiteta. Seriâ: Fiziko-Matematičeskie Nauki, 2019
In this paper, we study the accuracy of solving various differential equations describing the motion of large planets, the Moon and Sun. On the time interval from 31 years BC to 3969 AD, the numerical integration of Newtonian relativistic differential ...
Anatoliy Fedorovich Zausaev   +1 more
doaj   +1 more source

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