Perturbations of a spheroidal satellite due to direct solar radiation pressure

Moore, P.

doi:10.1007/bf01230233

Cited by 7 publications

(2 citation statements)

References 5 publications

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“…[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]. Saha L.M.…”

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 effect due to direct solar radiation pressure exceeds that of atmospheric drag at a height of 800 Km with a force magnitude of 10 -5 dyne/cm ( [27] and [26]) and is particularly emphasized for balloon-type satellites for which the area to mass ratio is large. Certain such satellites changes shape from spherical to spheroidal shapes, producing a component of force at right angles to the Sun-satellite direction ( [18]). www.ijacsa.thesai.org…”

Section: Introductionmentioning

confidence: 99%

Prediction of Satellite Motion under the Effects of the Earth’s Gravity, Drag Force and Solar Radiation Pressure in terms of the KS-regularized Variables

Dwidar¹

2014

IJACSA

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This paper is concerned with an orbit prediction using one of the best regular theories (KS-regularized variables). Perturbations due to the Earth's gravitational field with axial symmetry up to the fourth order zonal harmonic, atmospheric drag (variation in density model with height) and solar radiation pressure are considered. Applications of the problem with a comparison between the perturbations effect will be illustrated by numerical and graphical example.

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