Universal symbolic expression for radial distance of conic motion

In the present paper, a universal symbolic expression for radial distance of conic motion in recursive power series form is developed. The importance of this analytical power series representation is that it is invariant under many operations because the result of addition, multiplication,...

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Main Authors: Sharaf M.A., Saad A.S., Alshaery A.A.
Format: Article
Language:English
Published: Astronomical Observatory, Department of Astronomy, Belgrade 2014-01-01
Series:Serbian Astronomical Journal
Subjects:
Online Access:http://www.doiserbia.nb.rs/img/doi/1450-698X/2014/1450-698X1489087S.pdf
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spelling doaj-06e3670201d84463a1ea11596b0966d82020-11-24T23:29:30ZengAstronomical Observatory, Department of Astronomy, BelgradeSerbian Astronomical Journal1450-698X1820-92892014-01-012014189879210.2298/SAJ1489087S1450-698X1489087SUniversal symbolic expression for radial distance of conic motionSharaf M.A.0Saad A.S.1Alshaery A.A.2King Abdulaziz University, Faculty of Science, Department of Astronomy, Jeddah, KSANational Research Institute of Astronomy and Geophysics, Department of Astronomy, Cairo, Egypt + Qassim University, Department of Mathematics, Preparatory Year, Buraidah, KSAKing Abdulaziz University, College of Science for Girls, Department of Mathematics, Jeddah, KSAIn the present paper, a universal symbolic expression for radial distance of conic motion in recursive power series form is developed. The importance of this analytical power series representation is that it is invariant under many operations because the result of addition, multiplication, exponentiation, integration, differentiation, etc. of a power series is also a power series. This is the fact that provides excellent flexibility in dealing with analytical, as well as computational developments of problems related to radial distance. For computational developments, a full recursive algorithm is developed for the series coefficients. An efficient method using the continued fraction theory is provided for series evolution, and two devices are proposed to secure the convergence when the time interval (t − t0) is large. In addition, the algorithm does not need the solution of Kepler’s equation and its variants for parabolic and hyperbolic orbits. Numerical applications of the algorithm are given for three orbits of different eccentricities; the results showed that it is accurate for any conic motion.http://www.doiserbia.nb.rs/img/doi/1450-698X/2014/1450-698X1489087S.pdfcelestial mechanics
collection DOAJ
language English
format Article
sources DOAJ
author Sharaf M.A.
Saad A.S.
Alshaery A.A.
spellingShingle Sharaf M.A.
Saad A.S.
Alshaery A.A.
Universal symbolic expression for radial distance of conic motion
Serbian Astronomical Journal
celestial mechanics
author_facet Sharaf M.A.
Saad A.S.
Alshaery A.A.
author_sort Sharaf M.A.
title Universal symbolic expression for radial distance of conic motion
title_short Universal symbolic expression for radial distance of conic motion
title_full Universal symbolic expression for radial distance of conic motion
title_fullStr Universal symbolic expression for radial distance of conic motion
title_full_unstemmed Universal symbolic expression for radial distance of conic motion
title_sort universal symbolic expression for radial distance of conic motion
publisher Astronomical Observatory, Department of Astronomy, Belgrade
series Serbian Astronomical Journal
issn 1450-698X
1820-9289
publishDate 2014-01-01
description In the present paper, a universal symbolic expression for radial distance of conic motion in recursive power series form is developed. The importance of this analytical power series representation is that it is invariant under many operations because the result of addition, multiplication, exponentiation, integration, differentiation, etc. of a power series is also a power series. This is the fact that provides excellent flexibility in dealing with analytical, as well as computational developments of problems related to radial distance. For computational developments, a full recursive algorithm is developed for the series coefficients. An efficient method using the continued fraction theory is provided for series evolution, and two devices are proposed to secure the convergence when the time interval (t − t0) is large. In addition, the algorithm does not need the solution of Kepler’s equation and its variants for parabolic and hyperbolic orbits. Numerical applications of the algorithm are given for three orbits of different eccentricities; the results showed that it is accurate for any conic motion.
topic celestial mechanics
url http://www.doiserbia.nb.rs/img/doi/1450-698X/2014/1450-698X1489087S.pdf
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