The effects of diffuse solar radiation on the motion of an artificial satellite

Brookes, C. J.; Ryland, F. C. E.

doi:10.1007/bf01228560

Cited by 8 publications

(2 citation statements)

References 10 publications

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“…and Ryland F.C.E. [2] observed the perturbations in orbital elemental that caused by diffuse radiation pressure. Moore P. [3] study the perturbation on spheroid satellite using the variation of the approach developed by Aksnes K. [4].…”

Section: Introductionmentioning

confidence: 99%

Solar Radiation Pressure Effects on the Orbital Elements of Artificial Earth Satellite

Izzet¹

2023

Tikrit J. Pure Sci.

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The solar radiation pressure is one of the non-conservative force perturbation effects on earth satellite. A method presented to calculate the effect of radiation pressure on orbital elements for different altitude of satellites, the necessary calculation down by using modern Mat lab computer language. Typical results presented for radiation effect at deferent values of area mass ratio(A/m), the computed results indicated that the orbital elements much affected by solar radiation at high value of area mass ratio, also the effect on high orbit satellite is much more than that on low orbit satellite. The study also include the solar radiation pressure at two different value of ascending node ( Ω = 00 and Ω = 1800 ).

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Section: Introductionmentioning

confidence: 99%

Solar Radiation Pressure Effects on the Orbital Elements of Artificial Earth Satellite

Izzet¹

2023

Tikrit J. Pure Sci.

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“…The study of the effect of direct solar radiation pressure on the orbits of the artificial satellites was discussed in a lot of literatures, starting from pioneering works of [1][2][3][4] and other of [5][6][7][8][9]. Also the theory of third body perturbations on an artificial satellite motion was developed by many authors in the past.…”

Section: Introductionmentioning

confidence: 99%

Analytical Solution for the Combined Solar Radiation Pressure and Luni- Solar Effects on the Orbits of High Altitude Satellites~!2010-02-02~!2010-02-16~!2010-06-11~!

Saad¹,

Khalil²,

Amin³

2010

TOAAJ

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A new analytical solution is obtained for the motion of high-altitude earth satellites. The basic idea is to study the joint effects of direct solar radiation pressure and the gravitation of the Earth, Moon and the Sun on the orbits of the satellites. The mathematical model includes the zonal harmonics of the geopotential effects up to 4 J. The order of magnitude of each perturbing term is assessed. The formulae for the all perturbations forces are obtained up to the fourth order (where the mean motion of the moon (~ 10-2) is considered a small quantity of first order). The short, intermediate and long-period terms are eliminated from the Hamiltonian using a perturbation technique based on the Lie-Deprit-Kamel transform through three canonical transformations. The solution is intended to be used for ephemeris predictions for orbiters whose orbital semimajor axes are in the range of 15000 to 70000 kms.

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Long-periodic and secular perturbations to the orbit of a spherical satellite due to direct solar radiation pressure

Harwood

Swinerd

1995

Celestial Mech Dyn Astr

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The effects of diffuse solar radiation on the motion of an artificial satellite

Cited by 8 publications

References 10 publications

Solar Radiation Pressure Effects on the Orbital Elements of Artificial Earth Satellite

Solar Radiation Pressure Effects on the Orbital Elements of Artificial Earth Satellite

Analytical Solution for the Combined Solar Radiation Pressure and Luni- Solar Effects on the Orbits of High Altitude Satellites~!2010-02-02~!2010-02-16~!2010-06-11~!

Long-periodic and secular perturbations to the orbit of a spherical satellite due to direct solar radiation pressure

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