Journal article 1116 views
Aircraft Control via Variable Cant-Angle Winglets
P Bourdin,
A Gatto,
M. I Friswell,
Michael Friswell
Journal of Aircraft, Volume: 45, Issue: 2, Pages: 414 - 423
Swansea University Author: Michael Friswell
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DOI (Published version): 10.2514/1.27720
Abstract
Aircraft Control via Variable Cant-Angle Winglets
Published in: | Journal of Aircraft |
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ISSN: | 0021-8669 1533-3868 |
Published: |
2008
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URI: | https://cronfa.swan.ac.uk/Record/cronfa5504 |
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<?xml version="1.0"?><rfc1807><datestamp>2015-05-07T08:45:37.6306544</datestamp><bib-version>v2</bib-version><id>5504</id><entry>2013-09-03</entry><title>Aircraft Control via Variable Cant-Angle Winglets</title><swanseaauthors><author><sid>5894777b8f9c6e64bde3568d68078d40</sid><firstname>Michael</firstname><surname>Friswell</surname><name>Michael Friswell</name><active>true</active><ethesisStudent>false</ethesisStudent></author></swanseaauthors><date>2013-09-03</date><deptcode>FGSEN</deptcode><abstract></abstract><type>Journal Article</type><journal>Journal of Aircraft</journal><volume>45</volume><journalNumber>2</journalNumber><paginationStart>414</paginationStart><paginationEnd>423</paginationEnd><publisher/><issnPrint>0021-8669</issnPrint><issnElectronic>1533-3868</issnElectronic><keywords/><publishedDay>31</publishedDay><publishedMonth>12</publishedMonth><publishedYear>2008</publishedYear><publishedDate>2008-12-31</publishedDate><doi>10.2514/1.27720</doi><url/><notes>This paper formed part of the Marie-Curie Excellence grant on morphing aircraft (1.94M euros, 2005-2008) and was the first to consider using active winglets as control effectors. The investigation highlighted that novel aircraft configurations departed from the standard flight control approach of decoupling degrees of freedom and required a system view of such aircraft. This system level thinking was vital to the concept of the ERC Advanced Investigator grant on morphing aircraft (2.5M euros, 2010-2015).</notes><college>COLLEGE NANME</college><department>Science and Engineering - Faculty</department><CollegeCode>COLLEGE CODE</CollegeCode><DepartmentCode>FGSEN</DepartmentCode><institution>Swansea University</institution><apcterm/><lastEdited>2015-05-07T08:45:37.6306544</lastEdited><Created>2013-09-03T06:07:49.0000000</Created><path><level id="1">Faculty of Science and Engineering</level><level id="2">School of Engineering and Applied Sciences - Uncategorised</level></path><authors><author><firstname>P</firstname><surname>Bourdin</surname><order>1</order></author><author><firstname>A</firstname><surname>Gatto</surname><order>2</order></author><author><firstname>M. I</firstname><surname>Friswell</surname><order>3</order></author><author><firstname>Michael</firstname><surname>Friswell</surname><order>4</order></author></authors><documents/><OutputDurs/></rfc1807> |
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2015-05-07T08:45:37.6306544 v2 5504 2013-09-03 Aircraft Control via Variable Cant-Angle Winglets 5894777b8f9c6e64bde3568d68078d40 Michael Friswell Michael Friswell true false 2013-09-03 FGSEN Journal Article Journal of Aircraft 45 2 414 423 0021-8669 1533-3868 31 12 2008 2008-12-31 10.2514/1.27720 This paper formed part of the Marie-Curie Excellence grant on morphing aircraft (1.94M euros, 2005-2008) and was the first to consider using active winglets as control effectors. The investigation highlighted that novel aircraft configurations departed from the standard flight control approach of decoupling degrees of freedom and required a system view of such aircraft. This system level thinking was vital to the concept of the ERC Advanced Investigator grant on morphing aircraft (2.5M euros, 2010-2015). COLLEGE NANME Science and Engineering - Faculty COLLEGE CODE FGSEN Swansea University 2015-05-07T08:45:37.6306544 2013-09-03T06:07:49.0000000 Faculty of Science and Engineering School of Engineering and Applied Sciences - Uncategorised P Bourdin 1 A Gatto 2 M. I Friswell 3 Michael Friswell 4 |
title |
Aircraft Control via Variable Cant-Angle Winglets |
spellingShingle |
Aircraft Control via Variable Cant-Angle Winglets Michael Friswell |
title_short |
Aircraft Control via Variable Cant-Angle Winglets |
title_full |
Aircraft Control via Variable Cant-Angle Winglets |
title_fullStr |
Aircraft Control via Variable Cant-Angle Winglets |
title_full_unstemmed |
Aircraft Control via Variable Cant-Angle Winglets |
title_sort |
Aircraft Control via Variable Cant-Angle Winglets |
author_id_str_mv |
5894777b8f9c6e64bde3568d68078d40 |
author_id_fullname_str_mv |
5894777b8f9c6e64bde3568d68078d40_***_Michael Friswell |
author |
Michael Friswell |
author2 |
P Bourdin A Gatto M. I Friswell Michael Friswell |
format |
Journal article |
container_title |
Journal of Aircraft |
container_volume |
45 |
container_issue |
2 |
container_start_page |
414 |
publishDate |
2008 |
institution |
Swansea University |
issn |
0021-8669 1533-3868 |
doi_str_mv |
10.2514/1.27720 |
college_str |
Faculty of Science and Engineering |
hierarchytype |
|
hierarchy_top_id |
facultyofscienceandengineering |
hierarchy_top_title |
Faculty of Science and Engineering |
hierarchy_parent_id |
facultyofscienceandengineering |
hierarchy_parent_title |
Faculty of Science and Engineering |
department_str |
School of Engineering and Applied Sciences - Uncategorised{{{_:::_}}}Faculty of Science and Engineering{{{_:::_}}}School of Engineering and Applied Sciences - Uncategorised |
document_store_str |
0 |
active_str |
0 |
published_date |
2008-12-31T03:06:36Z |
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1763749707078696960 |
score |
11.035634 |