Gust Energy Extraction for Mini and Micro Uninhabited Aerial Vehicles
This paper discusses energy extraction from atmospheric turbulence by small and micro uninhabited aerial vehicles. A nonlinear longitudinal dynamic model of a glider with elevators as the sole control input is used for the aircraft, and feedback control laws for energy extraction are discussed. An e...
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Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 2009-03, Vol.32 (2), p.464-473 |
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description | This paper discusses energy extraction from atmospheric turbulence by small and micro uninhabited aerial vehicles. A nonlinear longitudinal dynamic model of a glider with elevators as the sole control input is used for the aircraft, and feedback control laws for energy extraction are discussed. An expression for energy change with respect to distance for flight in a spatially varying wind field is derived, and this is used with measurements of wind speed and gradient to compute the state that maximizes the instantaneous gain in total energy. A state feedback controller uses elevator input to regulate states to the optimal values. The state feedback control law is computed using linear quadratic regulator synthesis, and the state and input weight matrices that maximize energy gain are found using a search method. Simulation results of flights through sinusoidal gust fields and random thermal fields show the performance of the proposed approach. [PUBLISHER ABSTRACT] |
doi_str_mv | 10.2514/1.37735 |
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A nonlinear longitudinal dynamic model of a glider with elevators as the sole control input is used for the aircraft, and feedback control laws for energy extraction are discussed. An expression for energy change with respect to distance for flight in a spatially varying wind field is derived, and this is used with measurements of wind speed and gradient to compute the state that maximizes the instantaneous gain in total energy. A state feedback controller uses elevator input to regulate states to the optimal values. The state feedback control law is computed using linear quadratic regulator synthesis, and the state and input weight matrices that maximize energy gain are found using a search method. Simulation results of flights through sinusoidal gust fields and random thermal fields show the performance of the proposed approach. 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Systems</topic><topic>Energy</topic><topic>Exact sciences and technology</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Optimal control</topic><topic>Physics</topic><topic>Solid dynamics (ballistics, collision, multibody system, stabilization...)</topic><topic>Solid mechanics</topic><topic>Unmanned aerial vehicles</topic><topic>Vehicles</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Langelaan, Jack W</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Electronics & Communications Abstracts</collection><collection>Mechanical & 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>Langelaan, Jack W</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Gust Energy Extraction for Mini and Micro Uninhabited Aerial Vehicles</atitle><jtitle>Journal of guidance, control, and dynamics</jtitle><date>2009-03-01</date><risdate>2009</risdate><volume>32</volume><issue>2</issue><spage>464</spage><epage>473</epage><pages>464-473</pages><issn>0731-5090</issn><eissn>1533-3884</eissn><coden>JGCODS</coden><abstract>This paper discusses energy extraction from atmospheric turbulence by small and micro uninhabited aerial vehicles. 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subjects | Aircraft Applied sciences Computer science control theory systems Control system synthesis Control theory. Systems Energy Exact sciences and technology Fundamental areas of phenomenology (including applications) Optimal control Physics Solid dynamics (ballistics, collision, multibody system, stabilization...) Solid mechanics Unmanned aerial vehicles Vehicles |
title | Gust Energy Extraction for Mini and Micro Uninhabited Aerial Vehicles |
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