2015
DOI: 10.1016/j.asr.2015.03.044
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Effects of plasma drag on low Earth orbiting satellites due to solar forcing induced perturbations and heating

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Cited by 17 publications
(11 citation statements)
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“…The strength of the surface magnetic field is inversely proportional to the energy content of the ring current, which increases during geomagnetic storms (Hamilton et al, 1988). The solar wind condition and the mentioned geomagnetic parameters are important for studying and understanding magnetosphere-ionosphere coupling and effects (Borovsky and Denton, 2006;Tsurutani et al, 2006;Kozyra et al, 2006;Weigel 2010;Nwankwo et al, , 2015. However, having provided a precise background of the parameters, we will concentrate mainly on how various aspects of diurnal VLF signal varies in response to geomagnetic activity and storm footprints in the D region ionosphere via these parameters, especially the Dst index.…”
Section: Data Descriptionmentioning
confidence: 99%
“…The strength of the surface magnetic field is inversely proportional to the energy content of the ring current, which increases during geomagnetic storms (Hamilton et al, 1988). The solar wind condition and the mentioned geomagnetic parameters are important for studying and understanding magnetosphere-ionosphere coupling and effects (Borovsky and Denton, 2006;Tsurutani et al, 2006;Kozyra et al, 2006;Weigel 2010;Nwankwo et al, , 2015. However, having provided a precise background of the parameters, we will concentrate mainly on how various aspects of diurnal VLF signal varies in response to geomagnetic activity and storm footprints in the D region ionosphere via these parameters, especially the Dst index.…”
Section: Data Descriptionmentioning
confidence: 99%
“…We formulated and solved a set of coupled differential equations in previous work, to obtain instantaneous position, velocity components and acceleration of typical LEO satellites under the influence of atmospheric drag force in orbit (e.g., [4,[10][11][12]). We used the spherical polar coordinate system (r, θ, ø) with origin at the center of the Earth, and assumed that the satellite always remains in the same plane (i.e., θ=constant) while changing its position through the azimuthal parameters (ø, ǿ).…”
Section: Modeling Atmospheric Drag Effect On Leo Satellites' Trajectorymentioning
confidence: 99%
“…Spacecrafts moving through atmospheric medium experience atmospheric drag force, which constantly takes energy away from the orbit [1][2][3]. Atmospheric drag is the strongest force affecting the motion of satellites in low Earth orbit (LEO) especially at altitudes <800 km [4]. Solar activity enhances atmospheric drag on Low Earth orbiting satellites (LEOSs) and their effects on the space systems can be profound depending on the severity of solar activity [3].…”
Section: Introductionmentioning
confidence: 99%
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“…During the geomagnetic storm, the Joule heating at auroral and subauroral regions makes more contributions to the increase of atmospheric density (Knipp et al, 2004). Therefore, the increased atmosphere density at storm periods can largely enhance the atmosphere drag force and perturb the trajectories of LEO satellites, leading to accelerated orbital decay for LEO (Lei et al, 2013;Nwankwo et al, 2015;Walterscheid, 1989). The drastic fluctuation of the atmosphere density will increase the difficulty of drag force modeling for LEO POD during geomagnetic storms.…”
Section: Introductionmentioning
confidence: 99%