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Adaptive Robust Control (ARC) for an altitude control of a quadrotor type UAV carrying an unknown payloads
This research deals with an altitude controller of a quadrotor type UAV with an unknown total mass of the structure. We assume that the uncertainty results from the flight mission in which the UAV carries unknown payloads. Since the quadrotor type UAV involves both translational and rotational motio...
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creator | Byung-Cheol Min Ji-Hyeon Hong Matson, E. T. |
description | This research deals with an altitude controller of a quadrotor type UAV with an unknown total mass of the structure. We assume that the uncertainty results from the flight mission in which the UAV carries unknown payloads. Since the quadrotor type UAV involves both translational and rotational motions due to its inherent dynamics, it is of importance to know accurate information on the vehicles the moment of inertia and the total mass in order to guarantee the UAVs attitude and position controls. An Adaptive Robust Control (ARC) is utilized to compensate for the parametric uncertainty. Then, Lyapunov based stability analysis shows that the proposed control design guarantees asymptotic tracking error for the UAVs altitude control. Numerical simulation results which are time-based are presented to illustrate the good tracking performance of the designed control law. |
format | conference_proceeding |
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T.</creator><creatorcontrib>Byung-Cheol Min ; Ji-Hyeon Hong ; Matson, E. T.</creatorcontrib><description>This research deals with an altitude controller of a quadrotor type UAV with an unknown total mass of the structure. We assume that the uncertainty results from the flight mission in which the UAV carries unknown payloads. Since the quadrotor type UAV involves both translational and rotational motions due to its inherent dynamics, it is of importance to know accurate information on the vehicles the moment of inertia and the total mass in order to guarantee the UAVs attitude and position controls. An Adaptive Robust Control (ARC) is utilized to compensate for the parametric uncertainty. Then, Lyapunov based stability analysis shows that the proposed control design guarantees asymptotic tracking error for the UAVs altitude control. 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Then, Lyapunov based stability analysis shows that the proposed control design guarantees asymptotic tracking error for the UAVs altitude control. Numerical simulation results which are time-based are presented to illustrate the good tracking performance of the designed control law.</description><subject>Adaptive Robust Control</subject><subject>Altitude control</subject><subject>ARC</subject><subject>Attitude control</subject><subject>Helicopters</subject><subject>Quadrotor</subject><subject>Robust control</subject><subject>Robustness</subject><subject>Rotors</subject><subject>UAV</subject><subject>Uncertainty</subject><issn>2093-7121</issn><isbn>1457708353</isbn><isbn>9781457708350</isbn><isbn>8993215030</isbn><isbn>9788993215038</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2011</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><recordid>eNotT0tLxDAYjLiC-_oFXnLUQyGvNs2xFF-wICyr1-VrkkrWmtQ0VfrvrbjDwBzmAXOBVqVSnNGccHKJVlTkUpKS53yBlowonknK6DXaDsOJzCgKRbhYolNloE_u2-J9aMYh4Tr4FEOHb6t9fYfbEDF4DF1yaTQW67MbWgz4awQTQ5ojaeotfq3esIYYJ-ff_0qj__Dhx-Mepi6AGTboqoVusNuzrtHh4f5QP2W7l8fnutplTpGUUcOAFEpZqqGVQjbW6txywZlpCsmoLHMmhOLEgNZQzk8a01I5I28In9-v0c3_rLPWHvvoPiFOx4KSmYT_AlERVBk</recordid><startdate>201110</startdate><enddate>201110</enddate><creator>Byung-Cheol Min</creator><creator>Ji-Hyeon Hong</creator><creator>Matson, E. T.</creator><general>IEEE</general><scope>6IE</scope><scope>6IL</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIL</scope></search><sort><creationdate>201110</creationdate><title>Adaptive Robust Control (ARC) for an altitude control of a quadrotor type UAV carrying an unknown payloads</title><author>Byung-Cheol Min ; Ji-Hyeon Hong ; Matson, E. T.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i90t-1d2a0699e1caf747beec5e3432db6721785244930dacca8006bdf177775b03503</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2011</creationdate><topic>Adaptive Robust Control</topic><topic>Altitude control</topic><topic>ARC</topic><topic>Attitude control</topic><topic>Helicopters</topic><topic>Quadrotor</topic><topic>Robust control</topic><topic>Robustness</topic><topic>Rotors</topic><topic>UAV</topic><topic>Uncertainty</topic><toplevel>online_resources</toplevel><creatorcontrib>Byung-Cheol Min</creatorcontrib><creatorcontrib>Ji-Hyeon Hong</creatorcontrib><creatorcontrib>Matson, E. T.</creatorcontrib><collection>IEEE Electronic Library (IEL) Conference Proceedings</collection><collection>IEEE Proceedings Order Plan All Online (POP All Online) 1998-present by volume</collection><collection>IEEE Xplore All Conference Proceedings</collection><collection>IEEE</collection><collection>IEEE Proceedings Order Plans (POP All) 1998-Present</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Byung-Cheol Min</au><au>Ji-Hyeon Hong</au><au>Matson, E. T.</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Adaptive Robust Control (ARC) for an altitude control of a quadrotor type UAV carrying an unknown payloads</atitle><btitle>2011 11th International Conference on Control, Automation and Systems</btitle><stitle>ICCAS</stitle><date>2011-10</date><risdate>2011</risdate><spage>1147</spage><epage>1151</epage><pages>1147-1151</pages><issn>2093-7121</issn><isbn>1457708353</isbn><isbn>9781457708350</isbn><eisbn>8993215030</eisbn><eisbn>9788993215038</eisbn><abstract>This research deals with an altitude controller of a quadrotor type UAV with an unknown total mass of the structure. We assume that the uncertainty results from the flight mission in which the UAV carries unknown payloads. Since the quadrotor type UAV involves both translational and rotational motions due to its inherent dynamics, it is of importance to know accurate information on the vehicles the moment of inertia and the total mass in order to guarantee the UAVs attitude and position controls. An Adaptive Robust Control (ARC) is utilized to compensate for the parametric uncertainty. Then, Lyapunov based stability analysis shows that the proposed control design guarantees asymptotic tracking error for the UAVs altitude control. Numerical simulation results which are time-based are presented to illustrate the good tracking performance of the designed control law.</abstract><pub>IEEE</pub><tpages>5</tpages></addata></record> |
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ispartof | 2011 11th International Conference on Control, Automation and Systems, 2011, p.1147-1151 |
issn | 2093-7121 |
language | eng |
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source | IEEE Electronic Library (IEL) Conference Proceedings |
subjects | Adaptive Robust Control Altitude control ARC Attitude control Helicopters Quadrotor Robust control Robustness Rotors UAV Uncertainty |
title | Adaptive Robust Control (ARC) for an altitude control of a quadrotor type UAV carrying an unknown payloads |
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