2013
DOI: 10.2514/1.56118
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Relative Motion Control For Two-Spacecraft Electrostatic Orbit Corrections

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Cited by 39 publications
(12 citation statements)
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“…Simpler methods such as the point charge approximation and finite sphere model that have been used for Coulomb charge control analysis in the past [19,25,30] are limited to line-of-site forces and incapable of predicting electrostatic torques. The recently developed Multi Sphere Model (MSM) [20] uses a set of conductive spheres throughout the geometry of a spacecraft to capture the 3D electrostatic effects.…”
Section: Multi-sphere Methodsmentioning
confidence: 99%
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“…Simpler methods such as the point charge approximation and finite sphere model that have been used for Coulomb charge control analysis in the past [19,25,30] are limited to line-of-site forces and incapable of predicting electrostatic torques. The recently developed Multi Sphere Model (MSM) [20] uses a set of conductive spheres throughout the geometry of a spacecraft to capture the 3D electrostatic effects.…”
Section: Multi-sphere Methodsmentioning
confidence: 99%
“…For example, if vehicle 1 is charged negatively using an ion emitter, and the ion emission is aimed at the second vehicle, the latter will charge positively and create an attractive electrostatic force. Such indirect charging is of great interest to electrostatic geostationary debris removal [24,25,36]. The following simple modification of the potential control in Eq.…”
Section: Control With Only Positive or Negative Potentialsmentioning
confidence: 99%
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