Control capability analysis for complex spacecraft thruster configurations

Abstract The set of forces and moments that can be generated by thrusters of a spacecraft is called the “control capability” with respect to the thruster configuration. If the control capability of a thruster configuration is adequate to fulfill a given space mission, we say this configuration is a...
Ausführliche Beschreibung

Gespeichert in:

Autor*in:	Wang, Min [verfasserIn] Xie, YongChun [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2010

Schlagwörter:	thruster configuration control capability

Übergeordnetes Werk:	Enthalten in: Science in China - Heidelberg : Springer, 1997, 53(2010), 8 vom: 15. Juli, Seite 2089-2096
Übergeordnetes Werk:	volume:53 ; year:2010 ; number:8 ; day:15 ; month:07 ; pages:2089-2096

Links:	Volltext

DOI / URN:	10.1007/s11431-010-3139-9

Katalog-ID:	SPR019266677

Internformat


LEADER	01000caa a22002652 4500
001	SPR019266677
003	DE-627
005	20220111065355.0
007	cr uuu---uuuuu
008	201006s2010 xx \|\|\|\|\|o 00\| \|\|eng c
024	7		\|a 10.1007/s11431-010-3139-9 \|2 doi
035			\|a (DE-627)SPR019266677
035			\|a (SPR)s11431-010-3139-9-e
040			\|a DE-627 \|b ger \|c DE-627 \|e rakwb
041			\|a eng
082	0	4	\|a 600 \|q ASE
082	0	4	\|a 600 \|q ASE
084			\|a 50.00 \|2 bkl
100	1		\|a Wang, Min \|e verfasserin \|4 aut
245	1	0	\|a Control capability analysis for complex spacecraft thruster configurations
264		1	\|c 2010
336			\|a Text \|b txt \|2 rdacontent
337			\|a Computermedien \|b c \|2 rdamedia
338			\|a Online-Ressource \|b cr \|2 rdacarrier
520			\|a Abstract The set of forces and moments that can be generated by thrusters of a spacecraft is called the “control capability” with respect to the thruster configuration. If the control capability of a thruster configuration is adequate to fulfill a given space mission, we say this configuration is a feasible one with respect to the task. This study proposed a new way to analyze the control capability of the complex thruster configuration. Precise mathematical definitions of feasibility were proposed, based on which a criterion to judge the feasibility of the thruster configuration was presented through calculating the shortest distance to the boundary of the controllable region as a function of the thruster configuration. Finally, control capability analysis for the complex thruster configuration based on its feasibility with respect to the space mission was given followed by a 2-D thruster configuration example to demonstrate its validity.
650		4	\|a thruster \|7 (dpeaa)DE-He213
650		4	\|a configuration \|7 (dpeaa)DE-He213
650		4	\|a control capability \|7 (dpeaa)DE-He213
700	1		\|a Xie, YongChun \|e verfasserin \|4 aut
773	0	8	\|i Enthalten in \|t Science in China \|d Heidelberg : Springer, 1997 \|g 53(2010), 8 vom: 15. Juli, Seite 2089-2096 \|w (DE-627)385614756 \|w (DE-600)2142897-9 \|x 1862-281X \|7 nnns
773	1	8	\|g volume:53 \|g year:2010 \|g number:8 \|g day:15 \|g month:07 \|g pages:2089-2096
856	4	0	\|u https://dx.doi.org/10.1007/s11431-010-3139-9 \|z lizenzpflichtig \|3 Volltext
912			\|a GBV_USEFLAG_A
912			\|a SYSFLAG_A
912			\|a GBV_SPRINGER
912			\|a GBV_ILN_20
912			\|a GBV_ILN_22
912			\|a GBV_ILN_23
912			\|a GBV_ILN_24
912			\|a GBV_ILN_31
912			\|a GBV_ILN_32
912			\|a GBV_ILN_39
912			\|a GBV_ILN_40
912			\|a GBV_ILN_60
912			\|a GBV_ILN_62
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_120
912			\|a GBV_ILN_138
912			\|a GBV_ILN_152
912			\|a GBV_ILN_161
912			\|a GBV_ILN_171
912			\|a GBV_ILN_187
912			\|a GBV_ILN_224
912			\|a GBV_ILN_250
912			\|a GBV_ILN_281
912			\|a GBV_ILN_285
912			\|a GBV_ILN_293
912			\|a GBV_ILN_370
912			\|a GBV_ILN_602
912			\|a GBV_ILN_702
936	b	k	\|a 50.00 \|q ASE
951			\|a AR
952			\|d 53 \|j 2010 \|e 8 \|b 15 \|c 07 \|h 2089-2096

Indexfelder

author_variant	m w mw y x yx
matchkey_str	article:1862281X:2010----::otocpbltaayifropesaerftr
hierarchy_sort_str	2010
bklnumber	50.00
publishDate	2010
allfields	10.1007/s11431-010-3139-9 doi (DE-627)SPR019266677 (SPR)s11431-010-3139-9-e DE-627 ger DE-627 rakwb eng 600 ASE 600 ASE 50.00 bkl Wang, Min verfasserin aut Control capability analysis for complex spacecraft thruster configurations 2010 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The set of forces and moments that can be generated by thrusters of a spacecraft is called the “control capability” with respect to the thruster configuration. If the control capability of a thruster configuration is adequate to fulfill a given space mission, we say this configuration is a feasible one with respect to the task. This study proposed a new way to analyze the control capability of the complex thruster configuration. Precise mathematical definitions of feasibility were proposed, based on which a criterion to judge the feasibility of the thruster configuration was presented through calculating the shortest distance to the boundary of the controllable region as a function of the thruster configuration. Finally, control capability analysis for the complex thruster configuration based on its feasibility with respect to the space mission was given followed by a 2-D thruster configuration example to demonstrate its validity. thruster (dpeaa)DE-He213 configuration (dpeaa)DE-He213 control capability (dpeaa)DE-He213 Xie, YongChun verfasserin aut Enthalten in Science in China Heidelberg : Springer, 1997 53(2010), 8 vom: 15. Juli, Seite 2089-2096 (DE-627)385614756 (DE-600)2142897-9 1862-281X nnns volume:53 year:2010 number:8 day:15 month:07 pages:2089-2096 https://dx.doi.org/10.1007/s11431-010-3139-9 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 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_120 GBV_ILN_138 GBV_ILN_152 GBV_ILN_161 GBV_ILN_171 GBV_ILN_187 GBV_ILN_224 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 50.00 ASE AR 53 2010 8 15 07 2089-2096
spelling	10.1007/s11431-010-3139-9 doi (DE-627)SPR019266677 (SPR)s11431-010-3139-9-e DE-627 ger DE-627 rakwb eng 600 ASE 600 ASE 50.00 bkl Wang, Min verfasserin aut Control capability analysis for complex spacecraft thruster configurations 2010 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The set of forces and moments that can be generated by thrusters of a spacecraft is called the “control capability” with respect to the thruster configuration. If the control capability of a thruster configuration is adequate to fulfill a given space mission, we say this configuration is a feasible one with respect to the task. This study proposed a new way to analyze the control capability of the complex thruster configuration. Precise mathematical definitions of feasibility were proposed, based on which a criterion to judge the feasibility of the thruster configuration was presented through calculating the shortest distance to the boundary of the controllable region as a function of the thruster configuration. Finally, control capability analysis for the complex thruster configuration based on its feasibility with respect to the space mission was given followed by a 2-D thruster configuration example to demonstrate its validity. thruster (dpeaa)DE-He213 configuration (dpeaa)DE-He213 control capability (dpeaa)DE-He213 Xie, YongChun verfasserin aut Enthalten in Science in China Heidelberg : Springer, 1997 53(2010), 8 vom: 15. Juli, Seite 2089-2096 (DE-627)385614756 (DE-600)2142897-9 1862-281X nnns volume:53 year:2010 number:8 day:15 month:07 pages:2089-2096 https://dx.doi.org/10.1007/s11431-010-3139-9 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 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_120 GBV_ILN_138 GBV_ILN_152 GBV_ILN_161 GBV_ILN_171 GBV_ILN_187 GBV_ILN_224 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 50.00 ASE AR 53 2010 8 15 07 2089-2096
allfields_unstemmed	10.1007/s11431-010-3139-9 doi (DE-627)SPR019266677 (SPR)s11431-010-3139-9-e DE-627 ger DE-627 rakwb eng 600 ASE 600 ASE 50.00 bkl Wang, Min verfasserin aut Control capability analysis for complex spacecraft thruster configurations 2010 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The set of forces and moments that can be generated by thrusters of a spacecraft is called the “control capability” with respect to the thruster configuration. If the control capability of a thruster configuration is adequate to fulfill a given space mission, we say this configuration is a feasible one with respect to the task. This study proposed a new way to analyze the control capability of the complex thruster configuration. Precise mathematical definitions of feasibility were proposed, based on which a criterion to judge the feasibility of the thruster configuration was presented through calculating the shortest distance to the boundary of the controllable region as a function of the thruster configuration. Finally, control capability analysis for the complex thruster configuration based on its feasibility with respect to the space mission was given followed by a 2-D thruster configuration example to demonstrate its validity. thruster (dpeaa)DE-He213 configuration (dpeaa)DE-He213 control capability (dpeaa)DE-He213 Xie, YongChun verfasserin aut Enthalten in Science in China Heidelberg : Springer, 1997 53(2010), 8 vom: 15. Juli, Seite 2089-2096 (DE-627)385614756 (DE-600)2142897-9 1862-281X nnns volume:53 year:2010 number:8 day:15 month:07 pages:2089-2096 https://dx.doi.org/10.1007/s11431-010-3139-9 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 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_120 GBV_ILN_138 GBV_ILN_152 GBV_ILN_161 GBV_ILN_171 GBV_ILN_187 GBV_ILN_224 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 50.00 ASE AR 53 2010 8 15 07 2089-2096
allfieldsGer	10.1007/s11431-010-3139-9 doi (DE-627)SPR019266677 (SPR)s11431-010-3139-9-e DE-627 ger DE-627 rakwb eng 600 ASE 600 ASE 50.00 bkl Wang, Min verfasserin aut Control capability analysis for complex spacecraft thruster configurations 2010 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The set of forces and moments that can be generated by thrusters of a spacecraft is called the “control capability” with respect to the thruster configuration. If the control capability of a thruster configuration is adequate to fulfill a given space mission, we say this configuration is a feasible one with respect to the task. This study proposed a new way to analyze the control capability of the complex thruster configuration. Precise mathematical definitions of feasibility were proposed, based on which a criterion to judge the feasibility of the thruster configuration was presented through calculating the shortest distance to the boundary of the controllable region as a function of the thruster configuration. Finally, control capability analysis for the complex thruster configuration based on its feasibility with respect to the space mission was given followed by a 2-D thruster configuration example to demonstrate its validity. thruster (dpeaa)DE-He213 configuration (dpeaa)DE-He213 control capability (dpeaa)DE-He213 Xie, YongChun verfasserin aut Enthalten in Science in China Heidelberg : Springer, 1997 53(2010), 8 vom: 15. Juli, Seite 2089-2096 (DE-627)385614756 (DE-600)2142897-9 1862-281X nnns volume:53 year:2010 number:8 day:15 month:07 pages:2089-2096 https://dx.doi.org/10.1007/s11431-010-3139-9 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 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_120 GBV_ILN_138 GBV_ILN_152 GBV_ILN_161 GBV_ILN_171 GBV_ILN_187 GBV_ILN_224 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 50.00 ASE AR 53 2010 8 15 07 2089-2096
allfieldsSound	10.1007/s11431-010-3139-9 doi (DE-627)SPR019266677 (SPR)s11431-010-3139-9-e DE-627 ger DE-627 rakwb eng 600 ASE 600 ASE 50.00 bkl Wang, Min verfasserin aut Control capability analysis for complex spacecraft thruster configurations 2010 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The set of forces and moments that can be generated by thrusters of a spacecraft is called the “control capability” with respect to the thruster configuration. If the control capability of a thruster configuration is adequate to fulfill a given space mission, we say this configuration is a feasible one with respect to the task. This study proposed a new way to analyze the control capability of the complex thruster configuration. Precise mathematical definitions of feasibility were proposed, based on which a criterion to judge the feasibility of the thruster configuration was presented through calculating the shortest distance to the boundary of the controllable region as a function of the thruster configuration. Finally, control capability analysis for the complex thruster configuration based on its feasibility with respect to the space mission was given followed by a 2-D thruster configuration example to demonstrate its validity. thruster (dpeaa)DE-He213 configuration (dpeaa)DE-He213 control capability (dpeaa)DE-He213 Xie, YongChun verfasserin aut Enthalten in Science in China Heidelberg : Springer, 1997 53(2010), 8 vom: 15. Juli, Seite 2089-2096 (DE-627)385614756 (DE-600)2142897-9 1862-281X nnns volume:53 year:2010 number:8 day:15 month:07 pages:2089-2096 https://dx.doi.org/10.1007/s11431-010-3139-9 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 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_120 GBV_ILN_138 GBV_ILN_152 GBV_ILN_161 GBV_ILN_171 GBV_ILN_187 GBV_ILN_224 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 50.00 ASE AR 53 2010 8 15 07 2089-2096
language	English
source	Enthalten in Science in China 53(2010), 8 vom: 15. Juli, Seite 2089-2096 volume:53 year:2010 number:8 day:15 month:07 pages:2089-2096
sourceStr	Enthalten in Science in China 53(2010), 8 vom: 15. Juli, Seite 2089-2096 volume:53 year:2010 number:8 day:15 month:07 pages:2089-2096
format_phy_str_mv	Article
institution	findex.gbv.de
topic_facet	thruster configuration control capability
dewey-raw	600
isfreeaccess_bool	false
container_title	Science in China
authorswithroles_txt_mv	Wang, Min @@aut@@ Xie, YongChun @@aut@@
publishDateDaySort_date	2010-07-15T00:00:00Z
hierarchy_top_id	385614756
dewey-sort	3600
id	SPR019266677
language_de	englisch
fullrecord	<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">SPR019266677</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20220111065355.0</controlfield><controlfield tag="007">cr uuu---uuuuu</controlfield><controlfield tag="008">201006s2010 xx \|\|\|\|\|o 00\| \|\|eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1007/s11431-010-3139-9</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)SPR019266677</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(SPR)s11431-010-3139-9-e</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">600</subfield><subfield code="q">ASE</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">600</subfield><subfield code="q">ASE</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">50.00</subfield><subfield code="2">bkl</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Wang, Min</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Control capability analysis for complex spacecraft thruster configurations</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2010</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">Computermedien</subfield><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Online-Ressource</subfield><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract The set of forces and moments that can be generated by thrusters of a spacecraft is called the “control capability” with respect to the thruster configuration. If the control capability of a thruster configuration is adequate to fulfill a given space mission, we say this configuration is a feasible one with respect to the task. This study proposed a new way to analyze the control capability of the complex thruster configuration. Precise mathematical definitions of feasibility were proposed, based on which a criterion to judge the feasibility of the thruster configuration was presented through calculating the shortest distance to the boundary of the controllable region as a function of the thruster configuration. Finally, control capability analysis for the complex thruster configuration based on its feasibility with respect to the space mission was given followed by a 2-D thruster configuration example to demonstrate its validity.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">thruster</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">configuration</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">control capability</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Xie, YongChun</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">Science in China</subfield><subfield code="d">Heidelberg : Springer, 1997</subfield><subfield code="g">53(2010), 8 vom: 15. Juli, Seite 2089-2096</subfield><subfield code="w">(DE-627)385614756</subfield><subfield code="w">(DE-600)2142897-9</subfield><subfield code="x">1862-281X</subfield><subfield code="7">nnns</subfield></datafield><datafield tag="773" ind1="1" ind2="8"><subfield code="g">volume:53</subfield><subfield code="g">year:2010</subfield><subfield code="g">number:8</subfield><subfield code="g">day:15</subfield><subfield code="g">month:07</subfield><subfield code="g">pages:2089-2096</subfield></datafield><datafield tag="856" ind1="4" ind2="0"><subfield code="u">https://dx.doi.org/10.1007/s11431-010-3139-9</subfield><subfield code="z">lizenzpflichtig</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_USEFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SYSFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_SPRINGER</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_20</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_22</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_23</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_24</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_31</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_32</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_39</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_40</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_60</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_62</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_65</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_69</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_70</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_73</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_74</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_90</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_95</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_100</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_105</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_110</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_120</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_138</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_152</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_161</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_171</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_187</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_224</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_250</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_281</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_285</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_293</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_370</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_602</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_702</subfield></datafield><datafield tag="936" ind1="b" ind2="k"><subfield code="a">50.00</subfield><subfield code="q">ASE</subfield></datafield><datafield tag="951" ind1=" " ind2=" "><subfield code="a">AR</subfield></datafield><datafield tag="952" ind1=" " ind2=" "><subfield code="d">53</subfield><subfield code="j">2010</subfield><subfield code="e">8</subfield><subfield code="b">15</subfield><subfield code="c">07</subfield><subfield code="h">2089-2096</subfield></datafield></record></collection>
author	Wang, Min
spellingShingle	Wang, Min ddc 600 bkl 50.00 misc thruster misc configuration misc control capability Control capability analysis for complex spacecraft thruster configurations
authorStr	Wang, Min
ppnlink_with_tag_str_mv	@@773@@(DE-627)385614756
format	electronic Article
dewey-ones	600 - Technology
delete_txt_mv	keep
author_role	aut aut
collection	springer
remote_str	true
illustrated	Not Illustrated
issn	1862-281X
topic_title	600 ASE 50.00 bkl Control capability analysis for complex spacecraft thruster configurations thruster (dpeaa)DE-He213 configuration (dpeaa)DE-He213 control capability (dpeaa)DE-He213
topic	ddc 600 bkl 50.00 misc thruster misc configuration misc control capability
topic_unstemmed	ddc 600 bkl 50.00 misc thruster misc configuration misc control capability
topic_browse	ddc 600 bkl 50.00 misc thruster misc configuration misc control capability
format_facet	Elektronische Aufsätze Aufsätze Elektronische Ressource
format_main_str_mv	Text Zeitschrift/Artikel
carriertype_str_mv	cr
hierarchy_parent_title	Science in China
hierarchy_parent_id	385614756
dewey-tens	600 - Technology
hierarchy_top_title	Science in China
isfreeaccess_txt	false
familylinks_str_mv	(DE-627)385614756 (DE-600)2142897-9
title	Control capability analysis for complex spacecraft thruster configurations
ctrlnum	(DE-627)SPR019266677 (SPR)s11431-010-3139-9-e
title_full	Control capability analysis for complex spacecraft thruster configurations
author_sort	Wang, Min
journal	Science in China
journalStr	Science in China
lang_code	eng
isOA_bool	false
dewey-hundreds	600 - Technology
recordtype	marc
publishDateSort	2010
contenttype_str_mv	txt
container_start_page	2089
author_browse	Wang, Min Xie, YongChun
container_volume	53
class	600 ASE 50.00 bkl
format_se	Elektronische Aufsätze
author-letter	Wang, Min
doi_str_mv	10.1007/s11431-010-3139-9
dewey-full	600
author2-role	verfasserin
title_sort	control capability analysis for complex spacecraft thruster configurations
title_auth	Control capability analysis for complex spacecraft thruster configurations
abstract	Abstract The set of forces and moments that can be generated by thrusters of a spacecraft is called the “control capability” with respect to the thruster configuration. If the control capability of a thruster configuration is adequate to fulfill a given space mission, we say this configuration is a feasible one with respect to the task. This study proposed a new way to analyze the control capability of the complex thruster configuration. Precise mathematical definitions of feasibility were proposed, based on which a criterion to judge the feasibility of the thruster configuration was presented through calculating the shortest distance to the boundary of the controllable region as a function of the thruster configuration. Finally, control capability analysis for the complex thruster configuration based on its feasibility with respect to the space mission was given followed by a 2-D thruster configuration example to demonstrate its validity.
abstractGer	Abstract The set of forces and moments that can be generated by thrusters of a spacecraft is called the “control capability” with respect to the thruster configuration. If the control capability of a thruster configuration is adequate to fulfill a given space mission, we say this configuration is a feasible one with respect to the task. This study proposed a new way to analyze the control capability of the complex thruster configuration. Precise mathematical definitions of feasibility were proposed, based on which a criterion to judge the feasibility of the thruster configuration was presented through calculating the shortest distance to the boundary of the controllable region as a function of the thruster configuration. Finally, control capability analysis for the complex thruster configuration based on its feasibility with respect to the space mission was given followed by a 2-D thruster configuration example to demonstrate its validity.
abstract_unstemmed	Abstract The set of forces and moments that can be generated by thrusters of a spacecraft is called the “control capability” with respect to the thruster configuration. If the control capability of a thruster configuration is adequate to fulfill a given space mission, we say this configuration is a feasible one with respect to the task. This study proposed a new way to analyze the control capability of the complex thruster configuration. Precise mathematical definitions of feasibility were proposed, based on which a criterion to judge the feasibility of the thruster configuration was presented through calculating the shortest distance to the boundary of the controllable region as a function of the thruster configuration. Finally, control capability analysis for the complex thruster configuration based on its feasibility with respect to the space mission was given followed by a 2-D thruster configuration example to demonstrate its validity.
collection_details	GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 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_120 GBV_ILN_138 GBV_ILN_152 GBV_ILN_161 GBV_ILN_171 GBV_ILN_187 GBV_ILN_224 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702
container_issue	8
title_short	Control capability analysis for complex spacecraft thruster configurations
url	https://dx.doi.org/10.1007/s11431-010-3139-9
remote_bool	true
author2	Xie, YongChun
author2Str	Xie, YongChun
ppnlink	385614756
mediatype_str_mv	c
isOA_txt	false
hochschulschrift_bool	false
doi_str	10.1007/s11431-010-3139-9
up_date	2024-07-04T00:53:33.664Z
_version_	1803607776867385344
fullrecord_marcxml	<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">SPR019266677</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20220111065355.0</controlfield><controlfield tag="007">cr uuu---uuuuu</controlfield><controlfield tag="008">201006s2010 xx \|\|\|\|\|o 00\| \|\|eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1007/s11431-010-3139-9</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)SPR019266677</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(SPR)s11431-010-3139-9-e</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">600</subfield><subfield code="q">ASE</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">600</subfield><subfield code="q">ASE</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">50.00</subfield><subfield code="2">bkl</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Wang, Min</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Control capability analysis for complex spacecraft thruster configurations</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2010</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">Computermedien</subfield><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Online-Ressource</subfield><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract The set of forces and moments that can be generated by thrusters of a spacecraft is called the “control capability” with respect to the thruster configuration. If the control capability of a thruster configuration is adequate to fulfill a given space mission, we say this configuration is a feasible one with respect to the task. This study proposed a new way to analyze the control capability of the complex thruster configuration. Precise mathematical definitions of feasibility were proposed, based on which a criterion to judge the feasibility of the thruster configuration was presented through calculating the shortest distance to the boundary of the controllable region as a function of the thruster configuration. Finally, control capability analysis for the complex thruster configuration based on its feasibility with respect to the space mission was given followed by a 2-D thruster configuration example to demonstrate its validity.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">thruster</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">configuration</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">control capability</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Xie, YongChun</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">Science in China</subfield><subfield code="d">Heidelberg : Springer, 1997</subfield><subfield code="g">53(2010), 8 vom: 15. Juli, Seite 2089-2096</subfield><subfield code="w">(DE-627)385614756</subfield><subfield code="w">(DE-600)2142897-9</subfield><subfield code="x">1862-281X</subfield><subfield code="7">nnns</subfield></datafield><datafield tag="773" ind1="1" ind2="8"><subfield code="g">volume:53</subfield><subfield code="g">year:2010</subfield><subfield code="g">number:8</subfield><subfield code="g">day:15</subfield><subfield code="g">month:07</subfield><subfield code="g">pages:2089-2096</subfield></datafield><datafield tag="856" ind1="4" ind2="0"><subfield code="u">https://dx.doi.org/10.1007/s11431-010-3139-9</subfield><subfield code="z">lizenzpflichtig</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_USEFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SYSFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_SPRINGER</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_20</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_22</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_23</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_24</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_31</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_32</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_39</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_40</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_60</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_62</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_65</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_69</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_70</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_73</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_74</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_90</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_95</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_100</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_105</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_110</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_120</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_138</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_152</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_161</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_171</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_187</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_224</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_250</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_281</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_285</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_293</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_370</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_602</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_702</subfield></datafield><datafield tag="936" ind1="b" ind2="k"><subfield code="a">50.00</subfield><subfield code="q">ASE</subfield></datafield><datafield tag="951" ind1=" " ind2=" "><subfield code="a">AR</subfield></datafield><datafield tag="952" ind1=" " ind2=" "><subfield code="d">53</subfield><subfield code="j">2010</subfield><subfield code="e">8</subfield><subfield code="b">15</subfield><subfield code="c">07</subfield><subfield code="h">2089-2096</subfield></datafield></record></collection>
score	7.400504

Nicht das Richtige dabei?

Schreiben Sie uns!

Control capability analysis for complex spacecraft thruster configurations

Nicht das Richtige dabei?

Zugang & Verfügbarkeit

Vorhandene Bände

Nicht das Richtige dabei?