Dual Satellite Coverage using Particle Swarm Optimization

dc.contributor.authorOjeda Romero, Juan Andreen
dc.contributor.committeechairPhilen, Michael K.en
dc.contributor.committeememberEarle, Gregory D.en
dc.contributor.committeememberSultan, Cornelen
dc.contributor.departmentAerospace and Ocean Engineeringen
dc.date.accessioned2014-10-30T08:00:28Zen
dc.date.available2014-10-30T08:00:28Zen
dc.date.issued2014-10-29en
dc.description.abstractA dual satellite system in a Low Earth Orbit, LEO, would be beneficial to study the electromagnetic occurrences in the magnetosphere and their contributions to the development of the aurora events in the Earth's lower atmosphere. An orbit configuration is sought that would increase the total time that both satellites are inside the auroral oval. Some additional objectives include minimizing the total fuel cost and the average angle between the satellites' radius vectors. This orbit configuration is developed using a series of instantaneous burns applied at each satellite's perigee. An analysis of the optimal solutions generated by a Particle Swarm Optimization method is completed using a cost function with different weights for the time, fuel, and angle terms. Three different scenarios are presented: a single burn case, a double burn case, and a four burn case. The results are calculated using two different orbital mechanics models: an unperturbed two-body simulation and a two-body simulation with added Earth's equatorial bulge effects. It is shown that the added perturbation reduces the total event time in the optimal solutions generated. Specific weights for the cost function are recommended for further studies.en
dc.description.degreeMaster of Scienceen
dc.format.mediumETDen
dc.identifier.othervt_gsexam:3907en
dc.identifier.urihttp://hdl.handle.net/10919/50627en
dc.publisherVirginia Techen
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.subjectparticle swarm optimizationen
dc.subjectspace weatheren
dc.subjectaurora borealisen
dc.subjectorbital mechanicsen
dc.subjectsatellite coverageen
dc.titleDual Satellite Coverage using Particle Swarm Optimizationen
dc.typeThesisen
thesis.degree.disciplineAerospace Engineeringen
thesis.degree.grantorVirginia Polytechnic Institute and State Universityen
thesis.degree.levelmastersen
thesis.degree.nameMaster of Scienceen

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