Velocity-based detumbling strategy for a post-capture tethered net system

Tether-net is known as a popular method to actively remove space debris. After successfully capturing a space debris object by a net, a tethered system consisting of a chaser satellite, a main tether and a target is formed. Since the most urgent and important task after capture is to avoid collision...
Ausführliche Beschreibung

Gespeichert in:

Autor*in:	Shan, Minghe [verfasserIn] Shi, Lingling [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2022

Schlagwörter:	Space debris removal Tethered system Detumbling control Fuel consumption estimation

Übergeordnetes Werk:	Enthalten in: Advances in space research - Amsterdam [u.a.] : Elsevier Science, 1981, 70, Seite 1336-1350
Übergeordnetes Werk:	volume:70 ; pages:1336-1350

DOI / URN:	10.1016/j.asr.2022.06.012

Katalog-ID:	ELV008217440

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520			\|a Tether-net is known as a popular method to actively remove space debris. After successfully capturing a space debris object by a net, a tethered system consisting of a chaser satellite, a main tether and a target is formed. Since the most urgent and important task after capture is to avoid collision between the chaser and the tumbling target, detumbling of the target via the force by the main tether has to be performed. In this paper, we propose a novel and simple detumbling strategy to effectively stabilize the tethered system by controlling the motion of the chaser. Comparing to a previously proposed tension-based detumbling strategy, this newly proposed velocity-based method is simpler and more practical. Moreover, the fuel consumption of the proposed method is only 1% that of the tension-based method for investigated scenarios. With the proposed detumbling strategy, we not only analyze the influence of the system configuration on the detumbling effectiveness, but also analyze the detumbling capability of the method, concluding that the velocity-based detumbling strategy is able to detumble a spinning target up to 1.5 rad/s under a specific configuration. In addition, the proposed method is found to be suitable for both light and massive target detumbling.
650		4	\|a Space debris removal
650		4	\|a Tethered system
650		4	\|a Detumbling control
650		4	\|a Fuel consumption estimation
700	1		\|a Shi, Lingling \|e verfasserin \|4 aut
773	0	8	\|i Enthalten in \|t Advances in space research \|d Amsterdam [u.a.] : Elsevier Science, 1981 \|g 70, Seite 1336-1350 \|h Online-Ressource \|w (DE-627)320626113 \|w (DE-600)2023311-5 \|w (DE-576)255629427 \|x 0273-1177 \|7 nnns
773	1	8	\|g volume:70 \|g pages:1336-1350
912			\|a GBV_USEFLAG_U
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912			\|a GBV_ILN_23
912			\|a GBV_ILN_24
912			\|a GBV_ILN_31
912			\|a GBV_ILN_32
912			\|a GBV_ILN_40
912			\|a GBV_ILN_60
912			\|a GBV_ILN_62
912			\|a GBV_ILN_63
912			\|a GBV_ILN_65
912			\|a GBV_ILN_69
912			\|a GBV_ILN_70
912			\|a GBV_ILN_73
912			\|a GBV_ILN_74
912			\|a GBV_ILN_90
912			\|a GBV_ILN_95
912			\|a GBV_ILN_100
912			\|a GBV_ILN_105
912			\|a GBV_ILN_110
912			\|a GBV_ILN_150
912			\|a GBV_ILN_151
912			\|a GBV_ILN_224
912			\|a GBV_ILN_370
912			\|a GBV_ILN_602
912			\|a GBV_ILN_702
912			\|a GBV_ILN_2003
912			\|a GBV_ILN_2004
912			\|a GBV_ILN_2005
912			\|a GBV_ILN_2011
912			\|a GBV_ILN_2014
912			\|a GBV_ILN_2015
912			\|a GBV_ILN_2020
912			\|a GBV_ILN_2021
912			\|a GBV_ILN_2025
912			\|a GBV_ILN_2027
912			\|a GBV_ILN_2034
912			\|a GBV_ILN_2038
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912			\|a GBV_ILN_2056
912			\|a GBV_ILN_2059
912			\|a GBV_ILN_2061
912			\|a GBV_ILN_2064
912			\|a GBV_ILN_2065
912			\|a GBV_ILN_2068
912			\|a GBV_ILN_2111
912			\|a GBV_ILN_2112
912			\|a GBV_ILN_2113
912			\|a GBV_ILN_2118
912			\|a GBV_ILN_2122
912			\|a GBV_ILN_2129
912			\|a GBV_ILN_2143
912			\|a GBV_ILN_2147
912			\|a GBV_ILN_2148
912			\|a GBV_ILN_2152
912			\|a GBV_ILN_2153
912			\|a GBV_ILN_2190
912			\|a GBV_ILN_2336
912			\|a GBV_ILN_2507
912			\|a GBV_ILN_2522
912			\|a GBV_ILN_4035
912			\|a GBV_ILN_4037
912			\|a GBV_ILN_4112
912			\|a GBV_ILN_4125
912			\|a GBV_ILN_4126
912			\|a GBV_ILN_4242
912			\|a GBV_ILN_4251
912			\|a GBV_ILN_4305
912			\|a GBV_ILN_4313
912			\|a GBV_ILN_4323
912			\|a GBV_ILN_4324
912			\|a GBV_ILN_4326
912			\|a GBV_ILN_4333
912			\|a GBV_ILN_4334
912			\|a GBV_ILN_4335
912			\|a GBV_ILN_4338
912			\|a GBV_ILN_4393
936	b	k	\|a 39.00 \|j Astronomie: Allgemeines
936	b	k	\|a 50.93 \|j Weltraumforschung
951			\|a AR
952			\|d 70 \|h 1336-1350

Indexfelder

author_variant	m s ms l s ls
matchkey_str	article:02731177:2022----::eoiyaedtmlnsrtgfrpscpu
hierarchy_sort_str	2022
bklnumber	39.00 50.93
publishDate	2022
allfields	10.1016/j.asr.2022.06.012 doi (DE-627)ELV008217440 (ELSEVIER)S0273-1177(22)00481-1 DE-627 ger DE-627 rda eng 520 620 DE-600 39.00 bkl 50.93 bkl Shan, Minghe verfasserin aut Velocity-based detumbling strategy for a post-capture tethered net system 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Tether-net is known as a popular method to actively remove space debris. After successfully capturing a space debris object by a net, a tethered system consisting of a chaser satellite, a main tether and a target is formed. Since the most urgent and important task after capture is to avoid collision between the chaser and the tumbling target, detumbling of the target via the force by the main tether has to be performed. In this paper, we propose a novel and simple detumbling strategy to effectively stabilize the tethered system by controlling the motion of the chaser. Comparing to a previously proposed tension-based detumbling strategy, this newly proposed velocity-based method is simpler and more practical. Moreover, the fuel consumption of the proposed method is only 1% that of the tension-based method for investigated scenarios. With the proposed detumbling strategy, we not only analyze the influence of the system configuration on the detumbling effectiveness, but also analyze the detumbling capability of the method, concluding that the velocity-based detumbling strategy is able to detumble a spinning target up to 1.5 rad/s under a specific configuration. In addition, the proposed method is found to be suitable for both light and massive target detumbling. Space debris removal Tethered system Detumbling control Fuel consumption estimation Shi, Lingling verfasserin aut Enthalten in Advances in space research Amsterdam [u.a.] : Elsevier Science, 1981 70, Seite 1336-1350 Online-Ressource (DE-627)320626113 (DE-600)2023311-5 (DE-576)255629427 0273-1177 nnns volume:70 pages:1336-1350 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 39.00 Astronomie: Allgemeines 50.93 Weltraumforschung AR 70 1336-1350
spelling	10.1016/j.asr.2022.06.012 doi (DE-627)ELV008217440 (ELSEVIER)S0273-1177(22)00481-1 DE-627 ger DE-627 rda eng 520 620 DE-600 39.00 bkl 50.93 bkl Shan, Minghe verfasserin aut Velocity-based detumbling strategy for a post-capture tethered net system 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Tether-net is known as a popular method to actively remove space debris. After successfully capturing a space debris object by a net, a tethered system consisting of a chaser satellite, a main tether and a target is formed. Since the most urgent and important task after capture is to avoid collision between the chaser and the tumbling target, detumbling of the target via the force by the main tether has to be performed. In this paper, we propose a novel and simple detumbling strategy to effectively stabilize the tethered system by controlling the motion of the chaser. Comparing to a previously proposed tension-based detumbling strategy, this newly proposed velocity-based method is simpler and more practical. Moreover, the fuel consumption of the proposed method is only 1% that of the tension-based method for investigated scenarios. With the proposed detumbling strategy, we not only analyze the influence of the system configuration on the detumbling effectiveness, but also analyze the detumbling capability of the method, concluding that the velocity-based detumbling strategy is able to detumble a spinning target up to 1.5 rad/s under a specific configuration. In addition, the proposed method is found to be suitable for both light and massive target detumbling. Space debris removal Tethered system Detumbling control Fuel consumption estimation Shi, Lingling verfasserin aut Enthalten in Advances in space research Amsterdam [u.a.] : Elsevier Science, 1981 70, Seite 1336-1350 Online-Ressource (DE-627)320626113 (DE-600)2023311-5 (DE-576)255629427 0273-1177 nnns volume:70 pages:1336-1350 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 39.00 Astronomie: Allgemeines 50.93 Weltraumforschung AR 70 1336-1350
allfields_unstemmed	10.1016/j.asr.2022.06.012 doi (DE-627)ELV008217440 (ELSEVIER)S0273-1177(22)00481-1 DE-627 ger DE-627 rda eng 520 620 DE-600 39.00 bkl 50.93 bkl Shan, Minghe verfasserin aut Velocity-based detumbling strategy for a post-capture tethered net system 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Tether-net is known as a popular method to actively remove space debris. After successfully capturing a space debris object by a net, a tethered system consisting of a chaser satellite, a main tether and a target is formed. Since the most urgent and important task after capture is to avoid collision between the chaser and the tumbling target, detumbling of the target via the force by the main tether has to be performed. In this paper, we propose a novel and simple detumbling strategy to effectively stabilize the tethered system by controlling the motion of the chaser. Comparing to a previously proposed tension-based detumbling strategy, this newly proposed velocity-based method is simpler and more practical. Moreover, the fuel consumption of the proposed method is only 1% that of the tension-based method for investigated scenarios. With the proposed detumbling strategy, we not only analyze the influence of the system configuration on the detumbling effectiveness, but also analyze the detumbling capability of the method, concluding that the velocity-based detumbling strategy is able to detumble a spinning target up to 1.5 rad/s under a specific configuration. In addition, the proposed method is found to be suitable for both light and massive target detumbling. Space debris removal Tethered system Detumbling control Fuel consumption estimation Shi, Lingling verfasserin aut Enthalten in Advances in space research Amsterdam [u.a.] : Elsevier Science, 1981 70, Seite 1336-1350 Online-Ressource (DE-627)320626113 (DE-600)2023311-5 (DE-576)255629427 0273-1177 nnns volume:70 pages:1336-1350 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 39.00 Astronomie: Allgemeines 50.93 Weltraumforschung AR 70 1336-1350
allfieldsGer	10.1016/j.asr.2022.06.012 doi (DE-627)ELV008217440 (ELSEVIER)S0273-1177(22)00481-1 DE-627 ger DE-627 rda eng 520 620 DE-600 39.00 bkl 50.93 bkl Shan, Minghe verfasserin aut Velocity-based detumbling strategy for a post-capture tethered net system 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Tether-net is known as a popular method to actively remove space debris. After successfully capturing a space debris object by a net, a tethered system consisting of a chaser satellite, a main tether and a target is formed. Since the most urgent and important task after capture is to avoid collision between the chaser and the tumbling target, detumbling of the target via the force by the main tether has to be performed. In this paper, we propose a novel and simple detumbling strategy to effectively stabilize the tethered system by controlling the motion of the chaser. Comparing to a previously proposed tension-based detumbling strategy, this newly proposed velocity-based method is simpler and more practical. Moreover, the fuel consumption of the proposed method is only 1% that of the tension-based method for investigated scenarios. With the proposed detumbling strategy, we not only analyze the influence of the system configuration on the detumbling effectiveness, but also analyze the detumbling capability of the method, concluding that the velocity-based detumbling strategy is able to detumble a spinning target up to 1.5 rad/s under a specific configuration. In addition, the proposed method is found to be suitable for both light and massive target detumbling. Space debris removal Tethered system Detumbling control Fuel consumption estimation Shi, Lingling verfasserin aut Enthalten in Advances in space research Amsterdam [u.a.] : Elsevier Science, 1981 70, Seite 1336-1350 Online-Ressource (DE-627)320626113 (DE-600)2023311-5 (DE-576)255629427 0273-1177 nnns volume:70 pages:1336-1350 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 39.00 Astronomie: Allgemeines 50.93 Weltraumforschung AR 70 1336-1350
allfieldsSound	10.1016/j.asr.2022.06.012 doi (DE-627)ELV008217440 (ELSEVIER)S0273-1177(22)00481-1 DE-627 ger DE-627 rda eng 520 620 DE-600 39.00 bkl 50.93 bkl Shan, Minghe verfasserin aut Velocity-based detumbling strategy for a post-capture tethered net system 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Tether-net is known as a popular method to actively remove space debris. After successfully capturing a space debris object by a net, a tethered system consisting of a chaser satellite, a main tether and a target is formed. Since the most urgent and important task after capture is to avoid collision between the chaser and the tumbling target, detumbling of the target via the force by the main tether has to be performed. In this paper, we propose a novel and simple detumbling strategy to effectively stabilize the tethered system by controlling the motion of the chaser. Comparing to a previously proposed tension-based detumbling strategy, this newly proposed velocity-based method is simpler and more practical. Moreover, the fuel consumption of the proposed method is only 1% that of the tension-based method for investigated scenarios. With the proposed detumbling strategy, we not only analyze the influence of the system configuration on the detumbling effectiveness, but also analyze the detumbling capability of the method, concluding that the velocity-based detumbling strategy is able to detumble a spinning target up to 1.5 rad/s under a specific configuration. In addition, the proposed method is found to be suitable for both light and massive target detumbling. Space debris removal Tethered system Detumbling control Fuel consumption estimation Shi, Lingling verfasserin aut Enthalten in Advances in space research Amsterdam [u.a.] : Elsevier Science, 1981 70, Seite 1336-1350 Online-Ressource (DE-627)320626113 (DE-600)2023311-5 (DE-576)255629427 0273-1177 nnns volume:70 pages:1336-1350 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 39.00 Astronomie: Allgemeines 50.93 Weltraumforschung AR 70 1336-1350
language	English
source	Enthalten in Advances in space research 70, Seite 1336-1350 volume:70 pages:1336-1350
sourceStr	Enthalten in Advances in space research 70, Seite 1336-1350 volume:70 pages:1336-1350
format_phy_str_mv	Article
bklname	Astronomie: Allgemeines Weltraumforschung
institution	findex.gbv.de
topic_facet	Space debris removal Tethered system Detumbling control Fuel consumption estimation
dewey-raw	520
isfreeaccess_bool	false
container_title	Advances in space research
authorswithroles_txt_mv	Shan, Minghe @@aut@@ Shi, Lingling @@aut@@
publishDateDaySort_date	2022-01-01T00:00:00Z
hierarchy_top_id	320626113
dewey-sort	3520
id	ELV008217440
language_de	englisch
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author	Shan, Minghe
spellingShingle	Shan, Minghe ddc 520 bkl 39.00 bkl 50.93 misc Space debris removal misc Tethered system misc Detumbling control misc Fuel consumption estimation Velocity-based detumbling strategy for a post-capture tethered net system
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topic_title	520 620 DE-600 39.00 bkl 50.93 bkl Velocity-based detumbling strategy for a post-capture tethered net system Space debris removal Tethered system Detumbling control Fuel consumption estimation
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title	Velocity-based detumbling strategy for a post-capture tethered net system
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title_full	Velocity-based detumbling strategy for a post-capture tethered net system
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title_sort	velocity-based detumbling strategy for a post-capture tethered net system
title_auth	Velocity-based detumbling strategy for a post-capture tethered net system
abstract	Tether-net is known as a popular method to actively remove space debris. After successfully capturing a space debris object by a net, a tethered system consisting of a chaser satellite, a main tether and a target is formed. Since the most urgent and important task after capture is to avoid collision between the chaser and the tumbling target, detumbling of the target via the force by the main tether has to be performed. In this paper, we propose a novel and simple detumbling strategy to effectively stabilize the tethered system by controlling the motion of the chaser. Comparing to a previously proposed tension-based detumbling strategy, this newly proposed velocity-based method is simpler and more practical. Moreover, the fuel consumption of the proposed method is only 1% that of the tension-based method for investigated scenarios. With the proposed detumbling strategy, we not only analyze the influence of the system configuration on the detumbling effectiveness, but also analyze the detumbling capability of the method, concluding that the velocity-based detumbling strategy is able to detumble a spinning target up to 1.5 rad/s under a specific configuration. In addition, the proposed method is found to be suitable for both light and massive target detumbling.
abstractGer	Tether-net is known as a popular method to actively remove space debris. After successfully capturing a space debris object by a net, a tethered system consisting of a chaser satellite, a main tether and a target is formed. Since the most urgent and important task after capture is to avoid collision between the chaser and the tumbling target, detumbling of the target via the force by the main tether has to be performed. In this paper, we propose a novel and simple detumbling strategy to effectively stabilize the tethered system by controlling the motion of the chaser. Comparing to a previously proposed tension-based detumbling strategy, this newly proposed velocity-based method is simpler and more practical. Moreover, the fuel consumption of the proposed method is only 1% that of the tension-based method for investigated scenarios. With the proposed detumbling strategy, we not only analyze the influence of the system configuration on the detumbling effectiveness, but also analyze the detumbling capability of the method, concluding that the velocity-based detumbling strategy is able to detumble a spinning target up to 1.5 rad/s under a specific configuration. In addition, the proposed method is found to be suitable for both light and massive target detumbling.
abstract_unstemmed	Tether-net is known as a popular method to actively remove space debris. After successfully capturing a space debris object by a net, a tethered system consisting of a chaser satellite, a main tether and a target is formed. Since the most urgent and important task after capture is to avoid collision between the chaser and the tumbling target, detumbling of the target via the force by the main tether has to be performed. In this paper, we propose a novel and simple detumbling strategy to effectively stabilize the tethered system by controlling the motion of the chaser. Comparing to a previously proposed tension-based detumbling strategy, this newly proposed velocity-based method is simpler and more practical. Moreover, the fuel consumption of the proposed method is only 1% that of the tension-based method for investigated scenarios. With the proposed detumbling strategy, we not only analyze the influence of the system configuration on the detumbling effectiveness, but also analyze the detumbling capability of the method, concluding that the velocity-based detumbling strategy is able to detumble a spinning target up to 1.5 rad/s under a specific configuration. In addition, the proposed method is found to be suitable for both light and massive target detumbling.
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title_short	Velocity-based detumbling strategy for a post-capture tethered net system
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up_date	2024-07-06T18:56:49.412Z
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Velocity-based detumbling strategy for a post-capture tethered net system

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Zugang & Verfügbarkeit

Vorhandene Bände

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