Loading…
An Adaptive Local Variational Iteration Method for Orbit Propagation in Astrodynamics Problems
In this paper, a highly accurate and efficient Adaptive Local Variational Iteration Method (ALVIM) is presented to fulfil the need of the astrodynamics society for fast and accurate computational methods for guidance and control. The analytical iteration formula of this method is derived by using a...
Saved in:
Published in: | The Journal of the astronautical sciences 2023-02, Vol.70 (1), Article 2 |
---|---|
Main Authors: | , , , , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites |
Online Access: | Get full text |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
cited_by | |
---|---|
cites | cdi_FETCH-LOGICAL-c242t-fb4858b3664157375a53eba4292b093fbe2fba8553c19c7d5bede310584bb9fa3 |
container_end_page | |
container_issue | 1 |
container_start_page | |
container_title | The Journal of the astronautical sciences |
container_volume | 70 |
creator | Wang, Xuechuan Elgohary, Tarek A. Zhang, Zhe Tasif, Tahsinul H. Feng, Haoyang Atluri, Satya N. |
description | In this paper, a highly accurate and efficient Adaptive Local Variational Iteration Method (ALVIM) is presented to fulfil the need of the astrodynamics society for fast and accurate computational methods for guidance and control. The analytical iteration formula of this method is derived by using a general form of the first order nonlinear differential equations, followed by straightforward discretization using Chebyshev polynomials and collocation. The resulting numerical algorithm is very concise and easy to use, only involving highly sparse matrix operations of addition and multiplication, and no inversion of the Jacobian is required. Apart from the simple yet efficient iteration formula, a straightforward adaptive scheme is introduced to refine the step size and the collocation nodes at each time segment. The presented adaptive method guarantees prescribed accuracy without manual tuning of the algorithm. The computational cost of ALVIM, in terms of functional evaluations, is 1–2 orders of magnitude lower than adaptive finite difference methods. Numerical results of a large amplitude pendulum, perturbed two-body problem, and three-body problem validate the high accuracy and efficiency of this easy-to-use adaptive method. |
doi_str_mv | 10.1007/s40295-023-00366-y |
format | article |
fullrecord | <record><control><sourceid>crossref_sprin</sourceid><recordid>TN_cdi_crossref_primary_10_1007_s40295_023_00366_y</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>10_1007_s40295_023_00366_y</sourcerecordid><originalsourceid>FETCH-LOGICAL-c242t-fb4858b3664157375a53eba4292b093fbe2fba8553c19c7d5bede310584bb9fa3</originalsourceid><addsrcrecordid>eNp9UMtOwzAQtBBIlMIPcPIPGPyIm-QYVTwqBZUDcMSyE7u4auLINkj5e5yGQ0-cdrQzs9oZAG4JviMY5_chw7TkCFOGMGarFRrPwIKSacVzcn6CL8FVCPskIrgkC_BZ9bBq5RDtj4a1a-QBfkhvZbSuT3gTtT9i-KLjl2uhcR5uvbIRvno3yN1M2nQkRO_asZedbcJEqoPuwjW4MPIQ9M3fXIL3x4e39TOqt0-bdVWjhmY0IqOyghcqPZ4RnrOcS860khktqcIlM0pTo2TBOWtI2eQtV7rVKQEvMqVKI9kS0Plu410IXhsxeNtJPwqCxdSQmBsSqSFxbEiMycRmU0jifqe92Ltvn2KH_1y_xMdrNw</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype></control><display><type>article</type><title>An Adaptive Local Variational Iteration Method for Orbit Propagation in Astrodynamics Problems</title><source>Springer Nature</source><creator>Wang, Xuechuan ; Elgohary, Tarek A. ; Zhang, Zhe ; Tasif, Tahsinul H. ; Feng, Haoyang ; Atluri, Satya N.</creator><creatorcontrib>Wang, Xuechuan ; Elgohary, Tarek A. ; Zhang, Zhe ; Tasif, Tahsinul H. ; Feng, Haoyang ; Atluri, Satya N.</creatorcontrib><description>In this paper, a highly accurate and efficient Adaptive Local Variational Iteration Method (ALVIM) is presented to fulfil the need of the astrodynamics society for fast and accurate computational methods for guidance and control. The analytical iteration formula of this method is derived by using a general form of the first order nonlinear differential equations, followed by straightforward discretization using Chebyshev polynomials and collocation. The resulting numerical algorithm is very concise and easy to use, only involving highly sparse matrix operations of addition and multiplication, and no inversion of the Jacobian is required. Apart from the simple yet efficient iteration formula, a straightforward adaptive scheme is introduced to refine the step size and the collocation nodes at each time segment. The presented adaptive method guarantees prescribed accuracy without manual tuning of the algorithm. The computational cost of ALVIM, in terms of functional evaluations, is 1–2 orders of magnitude lower than adaptive finite difference methods. Numerical results of a large amplitude pendulum, perturbed two-body problem, and three-body problem validate the high accuracy and efficiency of this easy-to-use adaptive method.</description><identifier>ISSN: 2195-0571</identifier><identifier>EISSN: 2195-0571</identifier><identifier>DOI: 10.1007/s40295-023-00366-y</identifier><language>eng</language><publisher>New York: Springer US</publisher><subject>Aerospace Technology and Astronautics ; Engineering ; Mathematical Applications in the Physical Sciences ; Original Article ; Space Exploration and Astronautics ; Space Sciences (including Extraterrestrial Physics</subject><ispartof>The Journal of the astronautical sciences, 2023-02, Vol.70 (1), Article 2</ispartof><rights>The Author(s), under exclusive licence to American Astronautical Society 2023. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c242t-fb4858b3664157375a53eba4292b093fbe2fba8553c19c7d5bede310584bb9fa3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>Wang, Xuechuan</creatorcontrib><creatorcontrib>Elgohary, Tarek A.</creatorcontrib><creatorcontrib>Zhang, Zhe</creatorcontrib><creatorcontrib>Tasif, Tahsinul H.</creatorcontrib><creatorcontrib>Feng, Haoyang</creatorcontrib><creatorcontrib>Atluri, Satya N.</creatorcontrib><title>An Adaptive Local Variational Iteration Method for Orbit Propagation in Astrodynamics Problems</title><title>The Journal of the astronautical sciences</title><addtitle>J Astronaut Sci</addtitle><description>In this paper, a highly accurate and efficient Adaptive Local Variational Iteration Method (ALVIM) is presented to fulfil the need of the astrodynamics society for fast and accurate computational methods for guidance and control. The analytical iteration formula of this method is derived by using a general form of the first order nonlinear differential equations, followed by straightforward discretization using Chebyshev polynomials and collocation. The resulting numerical algorithm is very concise and easy to use, only involving highly sparse matrix operations of addition and multiplication, and no inversion of the Jacobian is required. Apart from the simple yet efficient iteration formula, a straightforward adaptive scheme is introduced to refine the step size and the collocation nodes at each time segment. The presented adaptive method guarantees prescribed accuracy without manual tuning of the algorithm. The computational cost of ALVIM, in terms of functional evaluations, is 1–2 orders of magnitude lower than adaptive finite difference methods. Numerical results of a large amplitude pendulum, perturbed two-body problem, and three-body problem validate the high accuracy and efficiency of this easy-to-use adaptive method.</description><subject>Aerospace Technology and Astronautics</subject><subject>Engineering</subject><subject>Mathematical Applications in the Physical Sciences</subject><subject>Original Article</subject><subject>Space Exploration and Astronautics</subject><subject>Space Sciences (including Extraterrestrial Physics</subject><issn>2195-0571</issn><issn>2195-0571</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><recordid>eNp9UMtOwzAQtBBIlMIPcPIPGPyIm-QYVTwqBZUDcMSyE7u4auLINkj5e5yGQ0-cdrQzs9oZAG4JviMY5_chw7TkCFOGMGarFRrPwIKSacVzcn6CL8FVCPskIrgkC_BZ9bBq5RDtj4a1a-QBfkhvZbSuT3gTtT9i-KLjl2uhcR5uvbIRvno3yN1M2nQkRO_asZedbcJEqoPuwjW4MPIQ9M3fXIL3x4e39TOqt0-bdVWjhmY0IqOyghcqPZ4RnrOcS860khktqcIlM0pTo2TBOWtI2eQtV7rVKQEvMqVKI9kS0Plu410IXhsxeNtJPwqCxdSQmBsSqSFxbEiMycRmU0jifqe92Ltvn2KH_1y_xMdrNw</recordid><startdate>20230209</startdate><enddate>20230209</enddate><creator>Wang, Xuechuan</creator><creator>Elgohary, Tarek A.</creator><creator>Zhang, Zhe</creator><creator>Tasif, Tahsinul H.</creator><creator>Feng, Haoyang</creator><creator>Atluri, Satya N.</creator><general>Springer US</general><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>20230209</creationdate><title>An Adaptive Local Variational Iteration Method for Orbit Propagation in Astrodynamics Problems</title><author>Wang, Xuechuan ; Elgohary, Tarek A. ; Zhang, Zhe ; Tasif, Tahsinul H. ; Feng, Haoyang ; Atluri, Satya N.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c242t-fb4858b3664157375a53eba4292b093fbe2fba8553c19c7d5bede310584bb9fa3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2023</creationdate><topic>Aerospace Technology and Astronautics</topic><topic>Engineering</topic><topic>Mathematical Applications in the Physical Sciences</topic><topic>Original Article</topic><topic>Space Exploration and Astronautics</topic><topic>Space Sciences (including Extraterrestrial Physics</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Wang, Xuechuan</creatorcontrib><creatorcontrib>Elgohary, Tarek A.</creatorcontrib><creatorcontrib>Zhang, Zhe</creatorcontrib><creatorcontrib>Tasif, Tahsinul H.</creatorcontrib><creatorcontrib>Feng, Haoyang</creatorcontrib><creatorcontrib>Atluri, Satya N.</creatorcontrib><collection>CrossRef</collection><jtitle>The Journal of the astronautical sciences</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Wang, Xuechuan</au><au>Elgohary, Tarek A.</au><au>Zhang, Zhe</au><au>Tasif, Tahsinul H.</au><au>Feng, Haoyang</au><au>Atluri, Satya N.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>An Adaptive Local Variational Iteration Method for Orbit Propagation in Astrodynamics Problems</atitle><jtitle>The Journal of the astronautical sciences</jtitle><stitle>J Astronaut Sci</stitle><date>2023-02-09</date><risdate>2023</risdate><volume>70</volume><issue>1</issue><artnum>2</artnum><issn>2195-0571</issn><eissn>2195-0571</eissn><abstract>In this paper, a highly accurate and efficient Adaptive Local Variational Iteration Method (ALVIM) is presented to fulfil the need of the astrodynamics society for fast and accurate computational methods for guidance and control. The analytical iteration formula of this method is derived by using a general form of the first order nonlinear differential equations, followed by straightforward discretization using Chebyshev polynomials and collocation. The resulting numerical algorithm is very concise and easy to use, only involving highly sparse matrix operations of addition and multiplication, and no inversion of the Jacobian is required. Apart from the simple yet efficient iteration formula, a straightforward adaptive scheme is introduced to refine the step size and the collocation nodes at each time segment. The presented adaptive method guarantees prescribed accuracy without manual tuning of the algorithm. The computational cost of ALVIM, in terms of functional evaluations, is 1–2 orders of magnitude lower than adaptive finite difference methods. Numerical results of a large amplitude pendulum, perturbed two-body problem, and three-body problem validate the high accuracy and efficiency of this easy-to-use adaptive method.</abstract><cop>New York</cop><pub>Springer US</pub><doi>10.1007/s40295-023-00366-y</doi></addata></record> |
fulltext | fulltext |
identifier | ISSN: 2195-0571 |
ispartof | The Journal of the astronautical sciences, 2023-02, Vol.70 (1), Article 2 |
issn | 2195-0571 2195-0571 |
language | eng |
recordid | cdi_crossref_primary_10_1007_s40295_023_00366_y |
source | Springer Nature |
subjects | Aerospace Technology and Astronautics Engineering Mathematical Applications in the Physical Sciences Original Article Space Exploration and Astronautics Space Sciences (including Extraterrestrial Physics |
title | An Adaptive Local Variational Iteration Method for Orbit Propagation in Astrodynamics Problems |
url | http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-07T13%3A24%3A41IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-crossref_sprin&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=An%20Adaptive%20Local%20Variational%20Iteration%20Method%20for%20Orbit%20Propagation%20in%20Astrodynamics%20Problems&rft.jtitle=The%20Journal%20of%20the%20astronautical%20sciences&rft.au=Wang,%20Xuechuan&rft.date=2023-02-09&rft.volume=70&rft.issue=1&rft.artnum=2&rft.issn=2195-0571&rft.eissn=2195-0571&rft_id=info:doi/10.1007/s40295-023-00366-y&rft_dat=%3Ccrossref_sprin%3E10_1007_s40295_023_00366_y%3C/crossref_sprin%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c242t-fb4858b3664157375a53eba4292b093fbe2fba8553c19c7d5bede310584bb9fa3%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |