Closed-Loop Optimization of Guidance Gain for Constrained Impact

Saved in:
Bibliographic Details
Published in:Journal of guidance, control, and dynamics control, and dynamics, 2017-02, Vol.40 (2), p.453-460
Main Authors: Liu, Xinfu, Shen, Zuojun, Lu, Ping
Format: Article
Language:English
Subjects:
Aeronautics
Aerospace engineering
Bias
Kinematics
Optimization
Velocity
Citations: Items that this one cites
Items that cite this one
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
cited_by cdi_FETCH-LOGICAL-c285t-34a8748e79c348d33f0d45035785cf7b67cb94c162268c65c6070af8ceb4b2423
cites cdi_FETCH-LOGICAL-c285t-34a8748e79c348d33f0d45035785cf7b67cb94c162268c65c6070af8ceb4b2423
container_end_page 460
container_issue 2
container_start_page 453
container_title Journal of guidance, control, and dynamics
container_volume 40
creator Liu, Xinfu
Shen, Zuojun
Lu, Ping
description
doi_str_mv 10.2514/1.G000323
format article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2494824110</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>4316421071</sourcerecordid><originalsourceid>FETCH-LOGICAL-c285t-34a8748e79c348d33f0d45035785cf7b67cb94c162268c65c6070af8ceb4b2423</originalsourceid><addsrcrecordid>eNp9kM9LwzAYhoMoOKcH_4OCJw-dX5IvP3pTitZBYRc9hzRNoGNratId9K93sp09vbzw8L7wEHJPYcUExSe6agCAM35BFlRwXnKt8ZIsQHFaCqjgmtzkvAWgXFK1IM_1Lmbfl22MU7GZ5mE__Nh5iGMRQ9Echt6OzheNHcYixFTUccxzOjbfF-v9ZN18S66C3WV_d84l-Xx7_ajfy3bTrOuXtnRMi7nkaLVC7VXlOOqe8wA9CuBCaeGC6qRyXYWOSsakdlI4CQps0M532DFkfEkeTrtTil8Hn2ezjYc0Hi8Nwwo1Q0rhP4pqBaxCiepIPZ4ol2LOyQczpWFv07ehYP40GmrOGvkvEl1hNQ</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>1870294647</pqid></control><display><type>article</type><title>Closed-Loop Optimization of Guidance Gain for Constrained Impact</title><source>Alma/SFX Local Collection</source><creator>Liu, Xinfu ; Shen, Zuojun ; Lu, Ping</creator><creatorcontrib>Liu, Xinfu ; Shen, Zuojun ; Lu, Ping</creatorcontrib><identifier>ISSN: 0731-5090</identifier><identifier>EISSN: 1533-3884</identifier><identifier>DOI: 10.2514/1.G000323</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Aeronautics ; Aerospace engineering ; Bias ; Kinematics ; Optimization ; Velocity</subject><ispartof>Journal of guidance, control, and dynamics, 2017-02, Vol.40 (2), p.453-460</ispartof><rights>Copyright © 2016 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. Copies of this paper may be made for personal and internal use, on condition that the copier pay the per-copy fee to the Copyright Clearance Center (CCC). All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0731-5090 (print) or 1533-3884 (online) to initiate your request.</rights><rights>Copyright © 2016 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. Copies of this paper may be made for personal and internal use, on condition that the copier pay the per-copy fee to the Copyright Clearance Center (CCC). All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0731-5090 (print) or 1533-3884 (online) to initiate your request.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c285t-34a8748e79c348d33f0d45035785cf7b67cb94c162268c65c6070af8ceb4b2423</citedby><cites>FETCH-LOGICAL-c285t-34a8748e79c348d33f0d45035785cf7b67cb94c162268c65c6070af8ceb4b2423</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,778,782,27911,27912</link.rule.ids></links><search><creatorcontrib>Liu, Xinfu</creatorcontrib><creatorcontrib>Shen, Zuojun</creatorcontrib><creatorcontrib>Lu, Ping</creatorcontrib><title>Closed-Loop Optimization of Guidance Gain for Constrained Impact</title><title>Journal of guidance, control, and dynamics</title><subject>Aeronautics</subject><subject>Aerospace engineering</subject><subject>Bias</subject><subject>Kinematics</subject><subject>Optimization</subject><subject>Velocity</subject><issn>0731-5090</issn><issn>1533-3884</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><recordid>eNp9kM9LwzAYhoMoOKcH_4OCJw-dX5IvP3pTitZBYRc9hzRNoGNratId9K93sp09vbzw8L7wEHJPYcUExSe6agCAM35BFlRwXnKt8ZIsQHFaCqjgmtzkvAWgXFK1IM_1Lmbfl22MU7GZ5mE__Nh5iGMRQ9Echt6OzheNHcYixFTUccxzOjbfF-v9ZN18S66C3WV_d84l-Xx7_ajfy3bTrOuXtnRMi7nkaLVC7VXlOOqe8wA9CuBCaeGC6qRyXYWOSsakdlI4CQps0M532DFkfEkeTrtTil8Hn2ezjYc0Hi8Nwwo1Q0rhP4pqBaxCiepIPZ4ol2LOyQczpWFv07ehYP40GmrOGvkvEl1hNQ</recordid><startdate>20170201</startdate><enddate>20170201</enddate><creator>Liu, Xinfu</creator><creator>Shen, Zuojun</creator><creator>Lu, Ping</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>7SP</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>JQ2</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope></search><sort><creationdate>20170201</creationdate><title>Closed-Loop Optimization of Guidance Gain for Constrained Impact</title><author>Liu, Xinfu ; Shen, Zuojun ; Lu, Ping</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c285t-34a8748e79c348d33f0d45035785cf7b67cb94c162268c65c6070af8ceb4b2423</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Aeronautics</topic><topic>Aerospace engineering</topic><topic>Bias</topic><topic>Kinematics</topic><topic>Optimization</topic><topic>Velocity</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Liu, Xinfu</creatorcontrib><creatorcontrib>Shen, Zuojun</creatorcontrib><creatorcontrib>Lu, Ping</creatorcontrib><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Electronics &amp; Communications Abstracts</collection><collection>Mechanical &amp; Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts – Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><jtitle>Journal of guidance, control, and dynamics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Liu, Xinfu</au><au>Shen, Zuojun</au><au>Lu, Ping</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Closed-Loop Optimization of Guidance Gain for Constrained Impact</atitle><jtitle>Journal of guidance, control, and dynamics</jtitle><date>2017-02-01</date><risdate>2017</risdate><volume>40</volume><issue>2</issue><spage>453</spage><epage>460</epage><pages>453-460</pages><issn>0731-5090</issn><eissn>1533-3884</eissn><cop>Reston</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.G000323</doi><tpages>8</tpages></addata></record>
fulltext fulltext
identifier ISSN: 0731-5090
ispartof Journal of guidance, control, and dynamics, 2017-02, Vol.40 (2), p.453-460
issn 0731-5090
1533-3884
language eng
recordid cdi_proquest_journals_2494824110
source Alma/SFX Local Collection
subjects Aeronautics
Aerospace engineering
Bias
Kinematics
Optimization
Velocity
title Closed-Loop Optimization of Guidance Gain for Constrained Impact
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-16T04%3A42%3A26IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Closed-Loop%20Optimization%20of%20Guidance%20Gain%20for%20Constrained%20Impact&rft.jtitle=Journal%20of%20guidance,%20control,%20and%20dynamics&rft.au=Liu,%20Xinfu&rft.date=2017-02-01&rft.volume=40&rft.issue=2&rft.spage=453&rft.epage=460&rft.pages=453-460&rft.issn=0731-5090&rft.eissn=1533-3884&rft_id=info:doi/10.2514/1.G000323&rft_dat=%3Cproquest_cross%3E4316421071%3C/proquest_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c285t-34a8748e79c348d33f0d45035785cf7b67cb94c162268c65c6070af8ceb4b2423%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=1870294647&rft_id=info:pmid/&rfr_iscdi=true