Control of quadcopter motion in the horizontal plane
This paper deals with trajectory tracking control of a quadcopter in a horizontal plane. A full rigid body model of the flying vehicle that doesn’t assume smallness of the Euler angles is considered. For synthesis of the tracking control the nonlinear dynamics inversion approach is used. Three diffe...
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| creator | Glazkov, T. V. Golubev, A. E. Gorbunov, A. V. Krishchenko, A. P. |
| description | This paper deals with trajectory tracking control of a quadcopter in a horizontal plane. A full rigid body model of the flying vehicle that doesn’t assume smallness of the Euler angles is considered. For synthesis of the tracking control the nonlinear dynamics inversion approach is used. Three different control strategies with restrictions on the orientation of the quadrotor are studied. |
| doi_str_mv | 10.1063/1.5114384 |
| format | Conference Proceeding |
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V. ; Golubev, A. E. ; Gorbunov, A. V. ; Krishchenko, A. P.</creator><contributor>Simos, Theodore ; Tsitouras, Charalambos</contributor><creatorcontrib>Glazkov, T. V. ; Golubev, A. E. ; Gorbunov, A. V. ; Krishchenko, A. P. ; Simos, Theodore ; Tsitouras, Charalambos</creatorcontrib><description>This paper deals with trajectory tracking control of a quadcopter in a horizontal plane. A full rigid body model of the flying vehicle that doesn’t assume smallness of the Euler angles is considered. For synthesis of the tracking control the nonlinear dynamics inversion approach is used. Three different control strategies with restrictions on the orientation of the quadrotor are studied.</description><identifier>ISSN: 0094-243X</identifier><identifier>EISSN: 1551-7616</identifier><identifier>DOI: 10.1063/1.5114384</identifier><identifier>CODEN: APCPCS</identifier><language>eng</language><publisher>Melville: American Institute of Physics</publisher><subject>Euler angles ; Nonlinear control ; Nonlinear dynamics ; Rigid structures ; Tracking control ; Trajectory control</subject><ispartof>AIP Conference Proceedings, 2019, Vol.2116 (1)</ispartof><rights>Author(s)</rights><rights>2019 Author(s). 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P.</creatorcontrib><title>Control of quadcopter motion in the horizontal plane</title><title>AIP Conference Proceedings</title><description>This paper deals with trajectory tracking control of a quadcopter in a horizontal plane. A full rigid body model of the flying vehicle that doesn’t assume smallness of the Euler angles is considered. For synthesis of the tracking control the nonlinear dynamics inversion approach is used. Three different control strategies with restrictions on the orientation of the quadrotor are studied.</description><subject>Euler angles</subject><subject>Nonlinear control</subject><subject>Nonlinear dynamics</subject><subject>Rigid structures</subject><subject>Tracking control</subject><subject>Trajectory control</subject><issn>0094-243X</issn><issn>1551-7616</issn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2019</creationdate><recordtype>conference_proceeding</recordtype><recordid>eNp9kMtKxDAYhYMoWEcXvkHAndAxf5LmspTiDQbcKLgLsU2YDp0mk6aCPr0dZsCdq7P5zoWD0DWQJRDB7mBZAXCm-AkqoKqglALEKSoI0byknH2co4tx3BBCtZSqQLwOQ06hx8Hj3WTbJsTsEt6G3IUBdwPOa4fXIXU_M2d7HHs7uEt05m0_uqujLtD748Nb_VyuXp9e6vtVGWnFcqmt5K7VTooGvFYatJfWNVqBZJ57RcFT0XLPKu6BCsKIV1LqT8u1ElJztkA3h9yYwm5yYzabMKVhrjSUCqqpmm0zdXugxqbLdr_bxNRtbfo2XyEZMMdHTGz9fzAQs7_wz8B-AdfoYR0</recordid><startdate>20190724</startdate><enddate>20190724</enddate><creator>Glazkov, T. V.</creator><creator>Golubev, A. E.</creator><creator>Gorbunov, A. V.</creator><creator>Krishchenko, A. P.</creator><general>American Institute of Physics</general><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20190724</creationdate><title>Control of quadcopter motion in the horizontal plane</title><author>Glazkov, T. V. ; Golubev, A. E. ; Gorbunov, A. V. ; Krishchenko, A. P.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-p253t-9a74ed9e76c1f98919f7aec98173f4f821f26d4f354f126030f8779ba49867943</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2019</creationdate><topic>Euler angles</topic><topic>Nonlinear control</topic><topic>Nonlinear dynamics</topic><topic>Rigid structures</topic><topic>Tracking control</topic><topic>Trajectory control</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Glazkov, T. V.</creatorcontrib><creatorcontrib>Golubev, A. E.</creatorcontrib><creatorcontrib>Gorbunov, A. V.</creatorcontrib><creatorcontrib>Krishchenko, A. P.</creatorcontrib><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Glazkov, T. V.</au><au>Golubev, A. E.</au><au>Gorbunov, A. V.</au><au>Krishchenko, A. P.</au><au>Simos, Theodore</au><au>Tsitouras, Charalambos</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Control of quadcopter motion in the horizontal plane</atitle><btitle>AIP Conference Proceedings</btitle><date>2019-07-24</date><risdate>2019</risdate><volume>2116</volume><issue>1</issue><issn>0094-243X</issn><eissn>1551-7616</eissn><coden>APCPCS</coden><abstract>This paper deals with trajectory tracking control of a quadcopter in a horizontal plane. A full rigid body model of the flying vehicle that doesn’t assume smallness of the Euler angles is considered. For synthesis of the tracking control the nonlinear dynamics inversion approach is used. Three different control strategies with restrictions on the orientation of the quadrotor are studied.</abstract><cop>Melville</cop><pub>American Institute of Physics</pub><doi>10.1063/1.5114384</doi><tpages>4</tpages></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 0094-243X |
| ispartof | AIP Conference Proceedings, 2019, Vol.2116 (1) |
| issn | 0094-243X 1551-7616 |
| language | eng |
| recordid | cdi_scitation_primary_10_1063_1_5114384 |
| source | AIP Journals Complete |
| subjects | Euler angles Nonlinear control Nonlinear dynamics Rigid structures Tracking control Trajectory control |
| title | Control of quadcopter motion in the horizontal plane |
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