Cislunar Navigation Constellation by Displaced Solar Sails

Increasing lunar exploration activities are giving rise to higher demands for a navigation constellation system in cislunar space. A novel constellation of solar sails around the Sun-Earth Artificial Lagrangian Points (ALPs) is proposed for cislunar navigation in this paper, which benefits from the...
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Autor*in:	Xiao Pan [verfasserIn] Ming Xu

Format:	Artikel
Sprache:	Englisch

Erschienen:	2017

Schlagwörter:	Feasibility studies Feasibility Communication Accuracy Architecture Trajectories Dilution Cislunar space Computer simulation Sun Exploration Navigation systems Geometric dilution of precision Working groups Astrophysics Orientation Equipment Mathematical models Earth Design optimization Sails Moon Navigation Stability Orbits Equilibrium Evolutionary algorithms Solar sails Lunar exploration

Übergeordnetes Werk:	Enthalten in: The journal of navigation - Cambridge : Univ. Press, 1972, 70(2017), 5, Seite 963
Übergeordnetes Werk:	volume:70 ; year:2017 ; number:5 ; pages:963

Links:	Volltext Link aufrufen

DOI / URN:	10.1017/S037346331700025X

Katalog-ID:	OLC1997178834

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245	1	0	\|a Cislunar Navigation Constellation by Displaced Solar Sails
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520			\|a Increasing lunar exploration activities are giving rise to higher demands for a navigation constellation system in cislunar space. A novel constellation of solar sails around the Sun-Earth Artificial Lagrangian Points (ALPs) is proposed for cislunar navigation in this paper, which benefits from the numberless and out-of-plane advantages of ALPs compared with the classical Lagrangian points. To relieve the technical pressure on sail equipment, a two-layer optimisation strategy including the navigation constellation architecture and trajectory design is developed to reduce the desired lightness number of the sail's motion. The constellation architecture is constructed in the shape of a regular tetrahedron, whose size and orientation are derived from the realisable lightness number at the ALPs. The powerful Hamiltonian structure-preserving controller and differential evolution algorithm are adopted to propagate the bounded quasi-periodic trajectory with minimum lightness number variation. With the premise of the sail's high feasibility in the mechanism, the numerical navigation simulations for a typical trans-lunar weak stability boundary trajectory indicate that the proposed navigation constellation has a low geometric dilution of precision factor and a good navigation performance.
650		4	\|a Feasibility studies
650		4	\|a Feasibility
650		4	\|a Communication
650		4	\|a Accuracy
650		4	\|a Architecture
650		4	\|a Trajectories
650		4	\|a Dilution
650		4	\|a Cislunar space
650		4	\|a Computer simulation
650		4	\|a Sun
650		4	\|a Exploration
650		4	\|a Navigation systems
650		4	\|a Geometric dilution of precision
650		4	\|a Working groups
650		4	\|a Astrophysics
650		4	\|a Orientation
650		4	\|a Equipment
650		4	\|a Mathematical models
650		4	\|a Earth
650		4	\|a Design optimization
650		4	\|a Sails
650		4	\|a Moon
650		4	\|a Navigation
650		4	\|a Stability
650		4	\|a Orbits
650		4	\|a Equilibrium
650		4	\|a Evolutionary algorithms
650		4	\|a Solar sails
650		4	\|a Lunar exploration
700	0		\|a Ming Xu \|4 oth
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author_variant	x p xp
matchkey_str	article:03734633:2017----::ilnraiainoseltobdsl
hierarchy_sort_str	2017
bklnumber	53.84 55.20 55.44 55.54 42.89 55.86
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allfields	10.1017/S037346331700025X doi PQ20171228 (DE-627)OLC1997178834 (DE-599)GBVOLC1997178834 (PRQ)p933-e52ae909f974b453f828ba223379a37b203c837e178bc69c22dd7ff4059ec0280 (KEY)0044480420170000070000500963cislunarnavigationconstellationbydisplacedsolarsai DE-627 ger DE-627 rakwb eng 380 DNB 53.84 bkl 55.20 bkl 55.44 bkl 55.54 bkl 42.89 bkl 55.86 bkl Xiao Pan verfasserin aut Cislunar Navigation Constellation by Displaced Solar Sails 2017 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier Increasing lunar exploration activities are giving rise to higher demands for a navigation constellation system in cislunar space. A novel constellation of solar sails around the Sun-Earth Artificial Lagrangian Points (ALPs) is proposed for cislunar navigation in this paper, which benefits from the numberless and out-of-plane advantages of ALPs compared with the classical Lagrangian points. To relieve the technical pressure on sail equipment, a two-layer optimisation strategy including the navigation constellation architecture and trajectory design is developed to reduce the desired lightness number of the sail's motion. The constellation architecture is constructed in the shape of a regular tetrahedron, whose size and orientation are derived from the realisable lightness number at the ALPs. The powerful Hamiltonian structure-preserving controller and differential evolution algorithm are adopted to propagate the bounded quasi-periodic trajectory with minimum lightness number variation. With the premise of the sail's high feasibility in the mechanism, the numerical navigation simulations for a typical trans-lunar weak stability boundary trajectory indicate that the proposed navigation constellation has a low geometric dilution of precision factor and a good navigation performance. Feasibility studies Feasibility Communication Accuracy Architecture Trajectories Dilution Cislunar space Computer simulation Sun Exploration Navigation systems Geometric dilution of precision Working groups Astrophysics Orientation Equipment Mathematical models Earth Design optimization Sails Moon Navigation Stability Orbits Equilibrium Evolutionary algorithms Solar sails Lunar exploration Ming Xu oth Enthalten in The journal of navigation Cambridge : Univ. Press, 1972 70(2017), 5, Seite 963 (DE-627)129297283 (DE-600)121410-X (DE-576)014490447 0373-4633 nnns volume:70 year:2017 number:5 pages:963 http://dx.doi.org/10.1017/S037346331700025X Volltext https://search.proquest.com/docview/1927238161 GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OPC-ARK GBV_ILN_70 GBV_ILN_160 GBV_ILN_162 53.84 AVZ 55.20 AVZ 55.44 AVZ 55.54 AVZ 42.89 AVZ 55.86 AVZ AR 70 2017 5 963
spelling	10.1017/S037346331700025X doi PQ20171228 (DE-627)OLC1997178834 (DE-599)GBVOLC1997178834 (PRQ)p933-e52ae909f974b453f828ba223379a37b203c837e178bc69c22dd7ff4059ec0280 (KEY)0044480420170000070000500963cislunarnavigationconstellationbydisplacedsolarsai DE-627 ger DE-627 rakwb eng 380 DNB 53.84 bkl 55.20 bkl 55.44 bkl 55.54 bkl 42.89 bkl 55.86 bkl Xiao Pan verfasserin aut Cislunar Navigation Constellation by Displaced Solar Sails 2017 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier Increasing lunar exploration activities are giving rise to higher demands for a navigation constellation system in cislunar space. A novel constellation of solar sails around the Sun-Earth Artificial Lagrangian Points (ALPs) is proposed for cislunar navigation in this paper, which benefits from the numberless and out-of-plane advantages of ALPs compared with the classical Lagrangian points. To relieve the technical pressure on sail equipment, a two-layer optimisation strategy including the navigation constellation architecture and trajectory design is developed to reduce the desired lightness number of the sail's motion. The constellation architecture is constructed in the shape of a regular tetrahedron, whose size and orientation are derived from the realisable lightness number at the ALPs. The powerful Hamiltonian structure-preserving controller and differential evolution algorithm are adopted to propagate the bounded quasi-periodic trajectory with minimum lightness number variation. With the premise of the sail's high feasibility in the mechanism, the numerical navigation simulations for a typical trans-lunar weak stability boundary trajectory indicate that the proposed navigation constellation has a low geometric dilution of precision factor and a good navigation performance. Feasibility studies Feasibility Communication Accuracy Architecture Trajectories Dilution Cislunar space Computer simulation Sun Exploration Navigation systems Geometric dilution of precision Working groups Astrophysics Orientation Equipment Mathematical models Earth Design optimization Sails Moon Navigation Stability Orbits Equilibrium Evolutionary algorithms Solar sails Lunar exploration Ming Xu oth Enthalten in The journal of navigation Cambridge : Univ. Press, 1972 70(2017), 5, Seite 963 (DE-627)129297283 (DE-600)121410-X (DE-576)014490447 0373-4633 nnns volume:70 year:2017 number:5 pages:963 http://dx.doi.org/10.1017/S037346331700025X Volltext https://search.proquest.com/docview/1927238161 GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OPC-ARK GBV_ILN_70 GBV_ILN_160 GBV_ILN_162 53.84 AVZ 55.20 AVZ 55.44 AVZ 55.54 AVZ 42.89 AVZ 55.86 AVZ AR 70 2017 5 963
allfields_unstemmed	10.1017/S037346331700025X doi PQ20171228 (DE-627)OLC1997178834 (DE-599)GBVOLC1997178834 (PRQ)p933-e52ae909f974b453f828ba223379a37b203c837e178bc69c22dd7ff4059ec0280 (KEY)0044480420170000070000500963cislunarnavigationconstellationbydisplacedsolarsai DE-627 ger DE-627 rakwb eng 380 DNB 53.84 bkl 55.20 bkl 55.44 bkl 55.54 bkl 42.89 bkl 55.86 bkl Xiao Pan verfasserin aut Cislunar Navigation Constellation by Displaced Solar Sails 2017 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier Increasing lunar exploration activities are giving rise to higher demands for a navigation constellation system in cislunar space. A novel constellation of solar sails around the Sun-Earth Artificial Lagrangian Points (ALPs) is proposed for cislunar navigation in this paper, which benefits from the numberless and out-of-plane advantages of ALPs compared with the classical Lagrangian points. To relieve the technical pressure on sail equipment, a two-layer optimisation strategy including the navigation constellation architecture and trajectory design is developed to reduce the desired lightness number of the sail's motion. The constellation architecture is constructed in the shape of a regular tetrahedron, whose size and orientation are derived from the realisable lightness number at the ALPs. The powerful Hamiltonian structure-preserving controller and differential evolution algorithm are adopted to propagate the bounded quasi-periodic trajectory with minimum lightness number variation. With the premise of the sail's high feasibility in the mechanism, the numerical navigation simulations for a typical trans-lunar weak stability boundary trajectory indicate that the proposed navigation constellation has a low geometric dilution of precision factor and a good navigation performance. Feasibility studies Feasibility Communication Accuracy Architecture Trajectories Dilution Cislunar space Computer simulation Sun Exploration Navigation systems Geometric dilution of precision Working groups Astrophysics Orientation Equipment Mathematical models Earth Design optimization Sails Moon Navigation Stability Orbits Equilibrium Evolutionary algorithms Solar sails Lunar exploration Ming Xu oth Enthalten in The journal of navigation Cambridge : Univ. Press, 1972 70(2017), 5, Seite 963 (DE-627)129297283 (DE-600)121410-X (DE-576)014490447 0373-4633 nnns volume:70 year:2017 number:5 pages:963 http://dx.doi.org/10.1017/S037346331700025X Volltext https://search.proquest.com/docview/1927238161 GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OPC-ARK GBV_ILN_70 GBV_ILN_160 GBV_ILN_162 53.84 AVZ 55.20 AVZ 55.44 AVZ 55.54 AVZ 42.89 AVZ 55.86 AVZ AR 70 2017 5 963
allfieldsGer	10.1017/S037346331700025X doi PQ20171228 (DE-627)OLC1997178834 (DE-599)GBVOLC1997178834 (PRQ)p933-e52ae909f974b453f828ba223379a37b203c837e178bc69c22dd7ff4059ec0280 (KEY)0044480420170000070000500963cislunarnavigationconstellationbydisplacedsolarsai DE-627 ger DE-627 rakwb eng 380 DNB 53.84 bkl 55.20 bkl 55.44 bkl 55.54 bkl 42.89 bkl 55.86 bkl Xiao Pan verfasserin aut Cislunar Navigation Constellation by Displaced Solar Sails 2017 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier Increasing lunar exploration activities are giving rise to higher demands for a navigation constellation system in cislunar space. A novel constellation of solar sails around the Sun-Earth Artificial Lagrangian Points (ALPs) is proposed for cislunar navigation in this paper, which benefits from the numberless and out-of-plane advantages of ALPs compared with the classical Lagrangian points. To relieve the technical pressure on sail equipment, a two-layer optimisation strategy including the navigation constellation architecture and trajectory design is developed to reduce the desired lightness number of the sail's motion. The constellation architecture is constructed in the shape of a regular tetrahedron, whose size and orientation are derived from the realisable lightness number at the ALPs. The powerful Hamiltonian structure-preserving controller and differential evolution algorithm are adopted to propagate the bounded quasi-periodic trajectory with minimum lightness number variation. With the premise of the sail's high feasibility in the mechanism, the numerical navigation simulations for a typical trans-lunar weak stability boundary trajectory indicate that the proposed navigation constellation has a low geometric dilution of precision factor and a good navigation performance. Feasibility studies Feasibility Communication Accuracy Architecture Trajectories Dilution Cislunar space Computer simulation Sun Exploration Navigation systems Geometric dilution of precision Working groups Astrophysics Orientation Equipment Mathematical models Earth Design optimization Sails Moon Navigation Stability Orbits Equilibrium Evolutionary algorithms Solar sails Lunar exploration Ming Xu oth Enthalten in The journal of navigation Cambridge : Univ. Press, 1972 70(2017), 5, Seite 963 (DE-627)129297283 (DE-600)121410-X (DE-576)014490447 0373-4633 nnns volume:70 year:2017 number:5 pages:963 http://dx.doi.org/10.1017/S037346331700025X Volltext https://search.proquest.com/docview/1927238161 GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OPC-ARK GBV_ILN_70 GBV_ILN_160 GBV_ILN_162 53.84 AVZ 55.20 AVZ 55.44 AVZ 55.54 AVZ 42.89 AVZ 55.86 AVZ AR 70 2017 5 963
allfieldsSound	10.1017/S037346331700025X doi PQ20171228 (DE-627)OLC1997178834 (DE-599)GBVOLC1997178834 (PRQ)p933-e52ae909f974b453f828ba223379a37b203c837e178bc69c22dd7ff4059ec0280 (KEY)0044480420170000070000500963cislunarnavigationconstellationbydisplacedsolarsai DE-627 ger DE-627 rakwb eng 380 DNB 53.84 bkl 55.20 bkl 55.44 bkl 55.54 bkl 42.89 bkl 55.86 bkl Xiao Pan verfasserin aut Cislunar Navigation Constellation by Displaced Solar Sails 2017 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier Increasing lunar exploration activities are giving rise to higher demands for a navigation constellation system in cislunar space. A novel constellation of solar sails around the Sun-Earth Artificial Lagrangian Points (ALPs) is proposed for cislunar navigation in this paper, which benefits from the numberless and out-of-plane advantages of ALPs compared with the classical Lagrangian points. To relieve the technical pressure on sail equipment, a two-layer optimisation strategy including the navigation constellation architecture and trajectory design is developed to reduce the desired lightness number of the sail's motion. The constellation architecture is constructed in the shape of a regular tetrahedron, whose size and orientation are derived from the realisable lightness number at the ALPs. The powerful Hamiltonian structure-preserving controller and differential evolution algorithm are adopted to propagate the bounded quasi-periodic trajectory with minimum lightness number variation. With the premise of the sail's high feasibility in the mechanism, the numerical navigation simulations for a typical trans-lunar weak stability boundary trajectory indicate that the proposed navigation constellation has a low geometric dilution of precision factor and a good navigation performance. Feasibility studies Feasibility Communication Accuracy Architecture Trajectories Dilution Cislunar space Computer simulation Sun Exploration Navigation systems Geometric dilution of precision Working groups Astrophysics Orientation Equipment Mathematical models Earth Design optimization Sails Moon Navigation Stability Orbits Equilibrium Evolutionary algorithms Solar sails Lunar exploration Ming Xu oth Enthalten in The journal of navigation Cambridge : Univ. Press, 1972 70(2017), 5, Seite 963 (DE-627)129297283 (DE-600)121410-X (DE-576)014490447 0373-4633 nnns volume:70 year:2017 number:5 pages:963 http://dx.doi.org/10.1017/S037346331700025X Volltext https://search.proquest.com/docview/1927238161 GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OPC-ARK GBV_ILN_70 GBV_ILN_160 GBV_ILN_162 53.84 AVZ 55.20 AVZ 55.44 AVZ 55.54 AVZ 42.89 AVZ 55.86 AVZ AR 70 2017 5 963
language	English
source	Enthalten in The journal of navigation 70(2017), 5, Seite 963 volume:70 year:2017 number:5 pages:963
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topic_facet	Feasibility studies Feasibility Communication Accuracy Architecture Trajectories Dilution Cislunar space Computer simulation Sun Exploration Navigation systems Geometric dilution of precision Working groups Astrophysics Orientation Equipment Mathematical models Earth Design optimization Sails Moon Navigation Stability Orbits Equilibrium Evolutionary algorithms Solar sails Lunar exploration
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author	Xiao Pan
spellingShingle	Xiao Pan ddc 380 bkl 53.84 bkl 55.20 bkl 55.44 bkl 55.54 bkl 42.89 bkl 55.86 misc Feasibility studies misc Feasibility misc Communication misc Accuracy misc Architecture misc Trajectories misc Dilution misc Cislunar space misc Computer simulation misc Sun misc Exploration misc Navigation systems misc Geometric dilution of precision misc Working groups misc Astrophysics misc Orientation misc Equipment misc Mathematical models misc Earth misc Design optimization misc Sails misc Moon misc Navigation misc Stability misc Orbits misc Equilibrium misc Evolutionary algorithms misc Solar sails misc Lunar exploration Cislunar Navigation Constellation by Displaced Solar Sails
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topic_title	380 DNB 53.84 bkl 55.20 bkl 55.44 bkl 55.54 bkl 42.89 bkl 55.86 bkl Cislunar Navigation Constellation by Displaced Solar Sails Feasibility studies Feasibility Communication Accuracy Architecture Trajectories Dilution Cislunar space Computer simulation Sun Exploration Navigation systems Geometric dilution of precision Working groups Astrophysics Orientation Equipment Mathematical models Earth Design optimization Sails Moon Navigation Stability Orbits Equilibrium Evolutionary algorithms Solar sails Lunar exploration
topic	ddc 380 bkl 53.84 bkl 55.20 bkl 55.44 bkl 55.54 bkl 42.89 bkl 55.86 misc Feasibility studies misc Feasibility misc Communication misc Accuracy misc Architecture misc Trajectories misc Dilution misc Cislunar space misc Computer simulation misc Sun misc Exploration misc Navigation systems misc Geometric dilution of precision misc Working groups misc Astrophysics misc Orientation misc Equipment misc Mathematical models misc Earth misc Design optimization misc Sails misc Moon misc Navigation misc Stability misc Orbits misc Equilibrium misc Evolutionary algorithms misc Solar sails misc Lunar exploration
topic_unstemmed	ddc 380 bkl 53.84 bkl 55.20 bkl 55.44 bkl 55.54 bkl 42.89 bkl 55.86 misc Feasibility studies misc Feasibility misc Communication misc Accuracy misc Architecture misc Trajectories misc Dilution misc Cislunar space misc Computer simulation misc Sun misc Exploration misc Navigation systems misc Geometric dilution of precision misc Working groups misc Astrophysics misc Orientation misc Equipment misc Mathematical models misc Earth misc Design optimization misc Sails misc Moon misc Navigation misc Stability misc Orbits misc Equilibrium misc Evolutionary algorithms misc Solar sails misc Lunar exploration
topic_browse	ddc 380 bkl 53.84 bkl 55.20 bkl 55.44 bkl 55.54 bkl 42.89 bkl 55.86 misc Feasibility studies misc Feasibility misc Communication misc Accuracy misc Architecture misc Trajectories misc Dilution misc Cislunar space misc Computer simulation misc Sun misc Exploration misc Navigation systems misc Geometric dilution of precision misc Working groups misc Astrophysics misc Orientation misc Equipment misc Mathematical models misc Earth misc Design optimization misc Sails misc Moon misc Navigation misc Stability misc Orbits misc Equilibrium misc Evolutionary algorithms misc Solar sails misc Lunar exploration
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title	Cislunar Navigation Constellation by Displaced Solar Sails
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title_full	Cislunar Navigation Constellation by Displaced Solar Sails
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title_sort	cislunar navigation constellation by displaced solar sails
title_auth	Cislunar Navigation Constellation by Displaced Solar Sails
abstract	Increasing lunar exploration activities are giving rise to higher demands for a navigation constellation system in cislunar space. A novel constellation of solar sails around the Sun-Earth Artificial Lagrangian Points (ALPs) is proposed for cislunar navigation in this paper, which benefits from the numberless and out-of-plane advantages of ALPs compared with the classical Lagrangian points. To relieve the technical pressure on sail equipment, a two-layer optimisation strategy including the navigation constellation architecture and trajectory design is developed to reduce the desired lightness number of the sail's motion. The constellation architecture is constructed in the shape of a regular tetrahedron, whose size and orientation are derived from the realisable lightness number at the ALPs. The powerful Hamiltonian structure-preserving controller and differential evolution algorithm are adopted to propagate the bounded quasi-periodic trajectory with minimum lightness number variation. With the premise of the sail's high feasibility in the mechanism, the numerical navigation simulations for a typical trans-lunar weak stability boundary trajectory indicate that the proposed navigation constellation has a low geometric dilution of precision factor and a good navigation performance.
abstractGer	Increasing lunar exploration activities are giving rise to higher demands for a navigation constellation system in cislunar space. A novel constellation of solar sails around the Sun-Earth Artificial Lagrangian Points (ALPs) is proposed for cislunar navigation in this paper, which benefits from the numberless and out-of-plane advantages of ALPs compared with the classical Lagrangian points. To relieve the technical pressure on sail equipment, a two-layer optimisation strategy including the navigation constellation architecture and trajectory design is developed to reduce the desired lightness number of the sail's motion. The constellation architecture is constructed in the shape of a regular tetrahedron, whose size and orientation are derived from the realisable lightness number at the ALPs. The powerful Hamiltonian structure-preserving controller and differential evolution algorithm are adopted to propagate the bounded quasi-periodic trajectory with minimum lightness number variation. With the premise of the sail's high feasibility in the mechanism, the numerical navigation simulations for a typical trans-lunar weak stability boundary trajectory indicate that the proposed navigation constellation has a low geometric dilution of precision factor and a good navigation performance.
abstract_unstemmed	Increasing lunar exploration activities are giving rise to higher demands for a navigation constellation system in cislunar space. A novel constellation of solar sails around the Sun-Earth Artificial Lagrangian Points (ALPs) is proposed for cislunar navigation in this paper, which benefits from the numberless and out-of-plane advantages of ALPs compared with the classical Lagrangian points. To relieve the technical pressure on sail equipment, a two-layer optimisation strategy including the navigation constellation architecture and trajectory design is developed to reduce the desired lightness number of the sail's motion. The constellation architecture is constructed in the shape of a regular tetrahedron, whose size and orientation are derived from the realisable lightness number at the ALPs. The powerful Hamiltonian structure-preserving controller and differential evolution algorithm are adopted to propagate the bounded quasi-periodic trajectory with minimum lightness number variation. With the premise of the sail's high feasibility in the mechanism, the numerical navigation simulations for a typical trans-lunar weak stability boundary trajectory indicate that the proposed navigation constellation has a low geometric dilution of precision factor and a good navigation performance.
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title_short	Cislunar Navigation Constellation by Displaced Solar Sails
url	http://dx.doi.org/10.1017/S037346331700025X https://search.proquest.com/docview/1927238161
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doi_str	10.1017/S037346331700025X
up_date	2024-07-04T02:21:37.929Z
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