Numerical study on Longitudinal control of Cessna 172 Skyhawk aircraft by Tail arm length
This paper covers a new method of longitudinally controlling an aircraft by changing the horizontal tail arm length, without the conventional control surface called 'elevator'. The effects of changing horizontal tail arm length from its steady level trimmed condition are determined numeric...
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| Veröffentlicht in: | IOP conference series. Materials Science and Engineering 2020-02, Vol.764 (1), p.12026 |
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| creator | Vadivelu, P Lakshmanan, D Naveen, R Mathivannan, K Yoges Kumar, G |
| description | This paper covers a new method of longitudinally controlling an aircraft by changing the horizontal tail arm length, without the conventional control surface called 'elevator'. The effects of changing horizontal tail arm length from its steady level trimmed condition are determined numerically for the chosen Cessna aircraft. From the numerical calculations, the possibilities of implementing this type of control in the chosen Cessna aircraft are analyzed. At last, some recommendations are suggested for the effective longitudinal control of the Cessna aircraft by changing horizontal tail arm length. Further, it is also suggested that employing both elevator control and tail arm length control together will make an aircraft to meet any kind of longitudinal controllability and stability requirement at any instant. This optimal aircraft configuration can be achieved by proposing a novel configuration and morphing solutions. |
| doi_str_mv | 10.1088/1757-899X/764/1/012026 |
| format | Article |
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This optimal aircraft configuration can be achieved by proposing a novel configuration and morphing solutions.</description><subject>Aircraft</subject><subject>Aircraft configurations</subject><subject>Aircraft control</subject><subject>Cessna aircraft</subject><subject>Control stability</subject><subject>Controllability</subject><subject>Elevators (control surfaces)</subject><subject>Longitudinal control</subject><subject>Morphing</subject><issn>1757-8981</issn><issn>1757-899X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2020</creationdate><recordtype>article</recordtype><sourceid>O3W</sourceid><sourceid>ABUWG</sourceid><sourceid>AFKRA</sourceid><sourceid>AZQEC</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><recordid>eNqFkF1LwzAUhoMoOKd_QQLeeDObpG2SXsqYHzD1YhP0KqRpsnXrmpq0SP-9GZWJIHiVk3Oe93B4ALjE6AYjziPMUjbhWfYWMZpEOEKYIEKPwOgwOD7UHJ-CM-83CFGWJGgE3p-7nXalkhX0bVf00NZwbutVGT5lHbrK1q2zFbQGTrX3tYSYEbjY9mv5uYWydMpJ08K8h0tZVlC6Hax0vWrX5-DEyMrri-93DF7vZsvpw2T-cv84vZ1PVEwInTBKETcqVYYXWS5VkcYsZyzTLE1xGhDGpOYF5wXVsuA6yYnBzCgUzpCc4HgMroa9jbMfnfat2NjOhdO9ICkNAOIZCxQdKOWs904b0bhyJ10vMBJ7jWJvSOxtiaBRYDFoDEEyBEvb_Gz-N3T9R-hpMfuFiaYw8RdYiYEu</recordid><startdate>20200201</startdate><enddate>20200201</enddate><creator>Vadivelu, P</creator><creator>Lakshmanan, D</creator><creator>Naveen, R</creator><creator>Mathivannan, K</creator><creator>Yoges Kumar, G</creator><general>IOP Publishing</general><scope>O3W</scope><scope>TSCCA</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>D1I</scope><scope>DWQXO</scope><scope>HCIFZ</scope><scope>KB.</scope><scope>L6V</scope><scope>M7S</scope><scope>PDBOC</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>PTHSS</scope></search><sort><creationdate>20200201</creationdate><title>Numerical study on Longitudinal control of Cessna 172 Skyhawk aircraft by Tail arm length</title><author>Vadivelu, P ; Lakshmanan, D ; Naveen, R ; Mathivannan, K ; Yoges Kumar, G</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c3226-76608fc5cf8d9bacd537b779e7551532277ae8d88d6ead8e4b2f17fc0172a8213</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2020</creationdate><topic>Aircraft</topic><topic>Aircraft configurations</topic><topic>Aircraft control</topic><topic>Cessna aircraft</topic><topic>Control stability</topic><topic>Controllability</topic><topic>Elevators (control surfaces)</topic><topic>Longitudinal control</topic><topic>Morphing</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Vadivelu, P</creatorcontrib><creatorcontrib>Lakshmanan, D</creatorcontrib><creatorcontrib>Naveen, R</creatorcontrib><creatorcontrib>Mathivannan, K</creatorcontrib><creatorcontrib>Yoges Kumar, G</creatorcontrib><collection>IOP Publishing Free Content</collection><collection>IOPscience (Open Access)</collection><collection>CrossRef</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central (Alumni Edition)</collection><collection>ProQuest Central UK/Ireland</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Materials Science Collection</collection><collection>ProQuest Central Korea</collection><collection>SciTech Premium Collection</collection><collection>Materials Science Database</collection><collection>ProQuest Engineering Collection</collection><collection>Engineering Database</collection><collection>Materials Science Collection</collection><collection>Publicly Available Content Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>Engineering Collection</collection><jtitle>IOP conference series. 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| subjects | Aircraft Aircraft configurations Aircraft control Cessna aircraft Control stability Controllability Elevators (control surfaces) Longitudinal control Morphing |
| title | Numerical study on Longitudinal control of Cessna 172 Skyhawk aircraft by Tail arm length |
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