Evolution of Orbital Parameters of Space Debris considering Orbital Maneuvers and Ground-Based Laser

Bibliographic Details
Main Author: Formiga, Jorge K.-S. [UNESP]
Publication Date: 2024
Other Authors: Santos, Denilson P.-S. [UNESP], Moraes, Rodolpho V. [UNESP], Prado, Antonio F.-B.-A.
Format: Conference object
Language: eng
Source: Repositório Institucional da UNESP
Download full: http://dx.doi.org/10.52202/078360-0189
https://hdl.handle.net/11449/297169
Summary: Space debris events are becoming increasingly common in regions where they reach a critical density, resulting in a heightened risk of collisions. Ground-based lasers, when precisely directed, can induce a propulsive effect that alters the perigee of particles, leading to their rapid incineration upon re-entry into Earth's atmosphere or facilitating orbital adjustments. Our objective was to assess the efficacy of such orbital maneuvers, accounting for both gravitational effects and the use of ground-based laser, as space debris—ranging from 1 cm to 10 cm in size and orbiting at altitudes between 100 and 1000 km—approaches Earth within a hypothetical heliocentric orbit. We conducted analyses by examining variations in orbital elements and energy following close approaches, employing single-pulse laser propulsion. Our analytical model considers factors such as laser fluence, debris attitude, and the relative motion between the laser and debris. Results indicate that the laser induces minor changes in ΔV, with a maximum energy efficiency, which can be accumulated to enhance re-entry energy. Consequently, it is possible to obtain a 30% increase in the variation of the orbital elements after the maneuver. Consequently, this study contributes a comprehensive examination of such maneuvers to the literature, highlighting their advantages over traditional orbital adjustments and delineating optimal conditions for collision avoidance and space debris mitigation. Enhancing the dynamic modelling and validating experimental outcomes is recommended to refine the understanding of these studies.
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spelling Evolution of Orbital Parameters of Space Debris considering Orbital Maneuvers and Ground-Based LaserAstrodynamicsGround-based laserOrbital elementsOrbital maneuversSpace DebrisSpace debris events are becoming increasingly common in regions where they reach a critical density, resulting in a heightened risk of collisions. Ground-based lasers, when precisely directed, can induce a propulsive effect that alters the perigee of particles, leading to their rapid incineration upon re-entry into Earth's atmosphere or facilitating orbital adjustments. Our objective was to assess the efficacy of such orbital maneuvers, accounting for both gravitational effects and the use of ground-based laser, as space debris—ranging from 1 cm to 10 cm in size and orbiting at altitudes between 100 and 1000 km—approaches Earth within a hypothetical heliocentric orbit. We conducted analyses by examining variations in orbital elements and energy following close approaches, employing single-pulse laser propulsion. Our analytical model considers factors such as laser fluence, debris attitude, and the relative motion between the laser and debris. Results indicate that the laser induces minor changes in ΔV, with a maximum energy efficiency, which can be accumulated to enhance re-entry energy. Consequently, it is possible to obtain a 30% increase in the variation of the orbital elements after the maneuver. Consequently, this study contributes a comprehensive examination of such maneuvers to the literature, highlighting their advantages over traditional orbital adjustments and delineating optimal conditions for collision avoidance and space debris mitigation. Enhancing the dynamic modelling and validating experimental outcomes is recommended to refine the understanding of these studies.São Paulo State University ICT/UNESP Institute of Science and TechnologySão Paulo State University UNESP, São João da Boa VistaSão Paulo State University UNESPNational Institute for Space Reseach- INPESão Paulo State University ICT/UNESP Institute of Science and TechnologySão Paulo State University UNESP, São João da Boa VistaSão Paulo State University UNESPUniversidade Estadual Paulista (UNESP)National Institute for Space Reseach- INPEFormiga, Jorge K.-S. [UNESP]Santos, Denilson P.-S. [UNESP]Moraes, Rodolpho V. [UNESP]Prado, Antonio F.-B.-A.2025-04-29T18:05:48Z2024-01-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/conferenceObject1952-1961http://dx.doi.org/10.52202/078360-0189Proceedings of the International Astronautical Congress, IAC, v. 3, p. 1952-1961.0074-1795https://hdl.handle.net/11449/29716910.52202/078360-01892-s2.0-85219186614Scopusreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengProceedings of the International Astronautical Congress, IACinfo:eu-repo/semantics/openAccess2025-04-30T14:28:38Zoai:repositorio.unesp.br:11449/297169Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestrepositoriounesp@unesp.bropendoar:29462025-04-30T14:28:38Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv Evolution of Orbital Parameters of Space Debris considering Orbital Maneuvers and Ground-Based Laser
title Evolution of Orbital Parameters of Space Debris considering Orbital Maneuvers and Ground-Based Laser
spellingShingle Evolution of Orbital Parameters of Space Debris considering Orbital Maneuvers and Ground-Based Laser
Formiga, Jorge K.-S. [UNESP]
Astrodynamics
Ground-based laser
Orbital elements
Orbital maneuvers
Space Debris
title_short Evolution of Orbital Parameters of Space Debris considering Orbital Maneuvers and Ground-Based Laser
title_full Evolution of Orbital Parameters of Space Debris considering Orbital Maneuvers and Ground-Based Laser
title_fullStr Evolution of Orbital Parameters of Space Debris considering Orbital Maneuvers and Ground-Based Laser
title_full_unstemmed Evolution of Orbital Parameters of Space Debris considering Orbital Maneuvers and Ground-Based Laser
title_sort Evolution of Orbital Parameters of Space Debris considering Orbital Maneuvers and Ground-Based Laser
author Formiga, Jorge K.-S. [UNESP]
author_facet Formiga, Jorge K.-S. [UNESP]
Santos, Denilson P.-S. [UNESP]
Moraes, Rodolpho V. [UNESP]
Prado, Antonio F.-B.-A.
author_role author
author2 Santos, Denilson P.-S. [UNESP]
Moraes, Rodolpho V. [UNESP]
Prado, Antonio F.-B.-A.
author2_role author
author
author
dc.contributor.none.fl_str_mv Universidade Estadual Paulista (UNESP)
National Institute for Space Reseach- INPE
dc.contributor.author.fl_str_mv Formiga, Jorge K.-S. [UNESP]
Santos, Denilson P.-S. [UNESP]
Moraes, Rodolpho V. [UNESP]
Prado, Antonio F.-B.-A.
dc.subject.por.fl_str_mv Astrodynamics
Ground-based laser
Orbital elements
Orbital maneuvers
Space Debris
topic Astrodynamics
Ground-based laser
Orbital elements
Orbital maneuvers
Space Debris
description Space debris events are becoming increasingly common in regions where they reach a critical density, resulting in a heightened risk of collisions. Ground-based lasers, when precisely directed, can induce a propulsive effect that alters the perigee of particles, leading to their rapid incineration upon re-entry into Earth's atmosphere or facilitating orbital adjustments. Our objective was to assess the efficacy of such orbital maneuvers, accounting for both gravitational effects and the use of ground-based laser, as space debris—ranging from 1 cm to 10 cm in size and orbiting at altitudes between 100 and 1000 km—approaches Earth within a hypothetical heliocentric orbit. We conducted analyses by examining variations in orbital elements and energy following close approaches, employing single-pulse laser propulsion. Our analytical model considers factors such as laser fluence, debris attitude, and the relative motion between the laser and debris. Results indicate that the laser induces minor changes in ΔV, with a maximum energy efficiency, which can be accumulated to enhance re-entry energy. Consequently, it is possible to obtain a 30% increase in the variation of the orbital elements after the maneuver. Consequently, this study contributes a comprehensive examination of such maneuvers to the literature, highlighting their advantages over traditional orbital adjustments and delineating optimal conditions for collision avoidance and space debris mitigation. Enhancing the dynamic modelling and validating experimental outcomes is recommended to refine the understanding of these studies.
publishDate 2024
dc.date.none.fl_str_mv 2024-01-01
2025-04-29T18:05:48Z
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.driver.fl_str_mv info:eu-repo/semantics/conferenceObject
format conferenceObject
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://dx.doi.org/10.52202/078360-0189
Proceedings of the International Astronautical Congress, IAC, v. 3, p. 1952-1961.
0074-1795
https://hdl.handle.net/11449/297169
10.52202/078360-0189
2-s2.0-85219186614
url http://dx.doi.org/10.52202/078360-0189
https://hdl.handle.net/11449/297169
identifier_str_mv Proceedings of the International Astronautical Congress, IAC, v. 3, p. 1952-1961.
0074-1795
10.52202/078360-0189
2-s2.0-85219186614
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Proceedings of the International Astronautical Congress, IAC
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv 1952-1961
dc.source.none.fl_str_mv Scopus
reponame:Repositório Institucional da UNESP
instname:Universidade Estadual Paulista (UNESP)
instacron:UNESP
instname_str Universidade Estadual Paulista (UNESP)
instacron_str UNESP
institution UNESP
reponame_str Repositório Institucional da UNESP
collection Repositório Institucional da UNESP
repository.name.fl_str_mv Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)
repository.mail.fl_str_mv repositoriounesp@unesp.br
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