Evolution of Orbital Parameters of Space Debris considering Orbital Maneuvers and Ground-Based Laser
Main Author: | |
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Publication Date: | 2024 |
Other Authors: | , , |
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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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 |
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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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1834482463410225152 |