Stochastic reachability for control of spacecraft relative motion
The concept of stochastic reachability allows for the assessment, before any maneuvers are initiated, of the probability of successfully implementing a rendezvous or docking procedure for spacecraft. The so-called reach-avoid problem lets us find the probability of reaching a target set while avoidi...
Gespeichert in:
Hauptverfasser: | , , |
---|---|
Format: | Tagungsbericht |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 4712 |
---|---|
container_issue | |
container_start_page | 4705 |
container_title | |
container_volume | |
creator | Lesser, Kendra Oishi, Meeko Erwin, R. Scott |
description | The concept of stochastic reachability allows for the assessment, before any maneuvers are initiated, of the probability of successfully implementing a rendezvous or docking procedure for spacecraft. The so-called reach-avoid problem lets us find the probability of reaching a target set while avoiding some unsafe or undesired set, despite uncertainty due to nonlinearity and disturbances. This paper examines two novel methods for the calculation of stochastic reachable sets, and specifically for rendezvous and docking problems. In particular, we examine a) particle (or scenario) approximations to expected values, and b) conversion of the reach-avoid probability to a chance-constrained convex optimization problem. Both methods allow for computation of the reach-avoid set in higher dimensions, as compared to other existing methods for computing stochastic reachable sets. We describe in detail both of these methods, and then apply them to spacecraft relative motion, a four-dimensional problem. |
doi_str_mv | 10.1109/CDC.2013.6760626 |
format | Conference Proceeding |
fullrecord | <record><control><sourceid>ieee_6IE</sourceid><recordid>TN_cdi_ieee_primary_6760626</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><ieee_id>6760626</ieee_id><sourcerecordid>6760626</sourcerecordid><originalsourceid>FETCH-LOGICAL-i217t-74efce08c0b4263595314dbaf8150cfc0ee432243daa07c96c4d4892ce46f9233</originalsourceid><addsrcrecordid>eNo1j01LAzEURSMq2NbuBTf5AzO-fMzLZFlGq0LBhboumTcJRqZNyQSh_96CdXXvgcuBy9idgFoIsA_dY1dLEKpGg4ASL9jSmlZoNKoxwqhLNv8HjVdsBsKKSkqBN2w-Td8A0ALijK3eS6IvN5VIPHt3qn0cYznykDKntC85jTwFPh0cecoulNNsdCX-eL5LJab9LbsObpz88pwL9rl--uheqs3b82u32lRRClMqo30gDy1BryWqxjZK6KF3oRUNUCDwXisptRqcA0MWSQ-6tZK8xmClUgt2_-eN3vvtIcedy8ft-b76BY-2TDQ</addsrcrecordid><sourcetype>Publisher</sourcetype><iscdi>true</iscdi><recordtype>conference_proceeding</recordtype></control><display><type>conference_proceeding</type><title>Stochastic reachability for control of spacecraft relative motion</title><source>IEEE Electronic Library (IEL) Conference Proceedings</source><creator>Lesser, Kendra ; Oishi, Meeko ; Erwin, R. Scott</creator><creatorcontrib>Lesser, Kendra ; Oishi, Meeko ; Erwin, R. Scott</creatorcontrib><description>The concept of stochastic reachability allows for the assessment, before any maneuvers are initiated, of the probability of successfully implementing a rendezvous or docking procedure for spacecraft. The so-called reach-avoid problem lets us find the probability of reaching a target set while avoiding some unsafe or undesired set, despite uncertainty due to nonlinearity and disturbances. This paper examines two novel methods for the calculation of stochastic reachable sets, and specifically for rendezvous and docking problems. In particular, we examine a) particle (or scenario) approximations to expected values, and b) conversion of the reach-avoid probability to a chance-constrained convex optimization problem. Both methods allow for computation of the reach-avoid set in higher dimensions, as compared to other existing methods for computing stochastic reachable sets. We describe in detail both of these methods, and then apply them to spacecraft relative motion, a four-dimensional problem.</description><identifier>ISSN: 0191-2216</identifier><identifier>ISBN: 1467357146</identifier><identifier>ISBN: 9781467357142</identifier><identifier>EISBN: 9781467357173</identifier><identifier>EISBN: 1479913812</identifier><identifier>EISBN: 1467357170</identifier><identifier>EISBN: 9781479913817</identifier><identifier>DOI: 10.1109/CDC.2013.6760626</identifier><language>eng</language><publisher>IEEE</publisher><subject>Approximation methods ; Dynamics ; Equations ; Mathematical model ; Noise ; Space vehicles ; Stochastic processes</subject><ispartof>52nd IEEE Conference on Decision and Control, 2013, p.4705-4712</ispartof><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/6760626$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>309,310,776,780,785,786,2052,27902,54895</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/6760626$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Lesser, Kendra</creatorcontrib><creatorcontrib>Oishi, Meeko</creatorcontrib><creatorcontrib>Erwin, R. Scott</creatorcontrib><title>Stochastic reachability for control of spacecraft relative motion</title><title>52nd IEEE Conference on Decision and Control</title><addtitle>CDC</addtitle><description>The concept of stochastic reachability allows for the assessment, before any maneuvers are initiated, of the probability of successfully implementing a rendezvous or docking procedure for spacecraft. The so-called reach-avoid problem lets us find the probability of reaching a target set while avoiding some unsafe or undesired set, despite uncertainty due to nonlinearity and disturbances. This paper examines two novel methods for the calculation of stochastic reachable sets, and specifically for rendezvous and docking problems. In particular, we examine a) particle (or scenario) approximations to expected values, and b) conversion of the reach-avoid probability to a chance-constrained convex optimization problem. Both methods allow for computation of the reach-avoid set in higher dimensions, as compared to other existing methods for computing stochastic reachable sets. We describe in detail both of these methods, and then apply them to spacecraft relative motion, a four-dimensional problem.</description><subject>Approximation methods</subject><subject>Dynamics</subject><subject>Equations</subject><subject>Mathematical model</subject><subject>Noise</subject><subject>Space vehicles</subject><subject>Stochastic processes</subject><issn>0191-2216</issn><isbn>1467357146</isbn><isbn>9781467357142</isbn><isbn>9781467357173</isbn><isbn>1479913812</isbn><isbn>1467357170</isbn><isbn>9781479913817</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2013</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNo1j01LAzEURSMq2NbuBTf5AzO-fMzLZFlGq0LBhboumTcJRqZNyQSh_96CdXXvgcuBy9idgFoIsA_dY1dLEKpGg4ASL9jSmlZoNKoxwqhLNv8HjVdsBsKKSkqBN2w-Td8A0ALijK3eS6IvN5VIPHt3qn0cYznykDKntC85jTwFPh0cecoulNNsdCX-eL5LJab9LbsObpz88pwL9rl--uheqs3b82u32lRRClMqo30gDy1BryWqxjZK6KF3oRUNUCDwXisptRqcA0MWSQ-6tZK8xmClUgt2_-eN3vvtIcedy8ft-b76BY-2TDQ</recordid><startdate>20130101</startdate><enddate>20130101</enddate><creator>Lesser, Kendra</creator><creator>Oishi, Meeko</creator><creator>Erwin, R. Scott</creator><general>IEEE</general><scope>6IE</scope><scope>6IH</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIO</scope></search><sort><creationdate>20130101</creationdate><title>Stochastic reachability for control of spacecraft relative motion</title><author>Lesser, Kendra ; Oishi, Meeko ; Erwin, R. Scott</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i217t-74efce08c0b4263595314dbaf8150cfc0ee432243daa07c96c4d4892ce46f9233</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2013</creationdate><topic>Approximation methods</topic><topic>Dynamics</topic><topic>Equations</topic><topic>Mathematical model</topic><topic>Noise</topic><topic>Space vehicles</topic><topic>Stochastic processes</topic><toplevel>online_resources</toplevel><creatorcontrib>Lesser, Kendra</creatorcontrib><creatorcontrib>Oishi, Meeko</creatorcontrib><creatorcontrib>Erwin, R. Scott</creatorcontrib><collection>IEEE Electronic Library (IEL) Conference Proceedings</collection><collection>IEEE Proceedings Order Plan (POP) 1998-present by volume</collection><collection>IEEE Xplore All Conference Proceedings</collection><collection>IEEE Electronic Library (IEL)</collection><collection>IEEE Proceedings Order Plans (POP) 1998-present</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Lesser, Kendra</au><au>Oishi, Meeko</au><au>Erwin, R. Scott</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Stochastic reachability for control of spacecraft relative motion</atitle><btitle>52nd IEEE Conference on Decision and Control</btitle><stitle>CDC</stitle><date>2013-01-01</date><risdate>2013</risdate><spage>4705</spage><epage>4712</epage><pages>4705-4712</pages><issn>0191-2216</issn><isbn>1467357146</isbn><isbn>9781467357142</isbn><eisbn>9781467357173</eisbn><eisbn>1479913812</eisbn><eisbn>1467357170</eisbn><eisbn>9781479913817</eisbn><abstract>The concept of stochastic reachability allows for the assessment, before any maneuvers are initiated, of the probability of successfully implementing a rendezvous or docking procedure for spacecraft. The so-called reach-avoid problem lets us find the probability of reaching a target set while avoiding some unsafe or undesired set, despite uncertainty due to nonlinearity and disturbances. This paper examines two novel methods for the calculation of stochastic reachable sets, and specifically for rendezvous and docking problems. In particular, we examine a) particle (or scenario) approximations to expected values, and b) conversion of the reach-avoid probability to a chance-constrained convex optimization problem. Both methods allow for computation of the reach-avoid set in higher dimensions, as compared to other existing methods for computing stochastic reachable sets. We describe in detail both of these methods, and then apply them to spacecraft relative motion, a four-dimensional problem.</abstract><pub>IEEE</pub><doi>10.1109/CDC.2013.6760626</doi><tpages>8</tpages><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | ISSN: 0191-2216 |
ispartof | 52nd IEEE Conference on Decision and Control, 2013, p.4705-4712 |
issn | 0191-2216 |
language | eng |
recordid | cdi_ieee_primary_6760626 |
source | IEEE Electronic Library (IEL) Conference Proceedings |
subjects | Approximation methods Dynamics Equations Mathematical model Noise Space vehicles Stochastic processes |
title | Stochastic reachability for control of spacecraft relative motion |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-31T11%3A05%3A05IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-ieee_6IE&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=proceeding&rft.atitle=Stochastic%20reachability%20for%20control%20of%20spacecraft%20relative%20motion&rft.btitle=52nd%20IEEE%20Conference%20on%20Decision%20and%20Control&rft.au=Lesser,%20Kendra&rft.date=2013-01-01&rft.spage=4705&rft.epage=4712&rft.pages=4705-4712&rft.issn=0191-2216&rft.isbn=1467357146&rft.isbn_list=9781467357142&rft_id=info:doi/10.1109/CDC.2013.6760626&rft_dat=%3Cieee_6IE%3E6760626%3C/ieee_6IE%3E%3Curl%3E%3C/url%3E&rft.eisbn=9781467357173&rft.eisbn_list=1479913812&rft.eisbn_list=1467357170&rft.eisbn_list=9781479913817&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rft_ieee_id=6760626&rfr_iscdi=true |