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You searched for subject:(adaptive wing). Showing records 1 – 15 of 15 total matches.

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University of Manchester

1. El Ouardi, Othman. Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism.

Degree: 2014, University of Manchester

Wing morphing has the potential to significantly improve the performance of an aircraft. The aerospace industry currently relies on control surfaces for changing aircraft wing(more)

Subjects/Keywords: Morphing wing; Adaptive wing; SMA; Variable thickness wing; Shape morphing; Smart materials

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

El Ouardi, O. (2014). Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:237682

Chicago Manual of Style (16th Edition):

El Ouardi, Othman. “Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism.” 2014. Doctoral Dissertation, University of Manchester. Accessed November 13, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:237682.

MLA Handbook (7th Edition):

El Ouardi, Othman. “Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism.” 2014. Web. 13 Nov 2019.

Vancouver:

El Ouardi O. Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism. [Internet] [Doctoral dissertation]. University of Manchester; 2014. [cited 2019 Nov 13]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:237682.

Council of Science Editors:

El Ouardi O. Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism. [Doctoral Dissertation]. University of Manchester; 2014. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:237682


University of Kansas

2. Schueler, Samantha Katelyn. A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions.

Degree: MS, Aerospace Engineering, 2014, University of Kansas

 In 2008, the commercial aerospace industry saw substantial reductions in aircraft operating hours because of the struggling economy and high operating costs. Recurring fuel costs… (more)

Subjects/Keywords: Aerospace engineering; Adaptive structures; Wing design

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APA (6th Edition):

Schueler, S. K. (2014). A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/19593

Chicago Manual of Style (16th Edition):

Schueler, Samantha Katelyn. “A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions.” 2014. Masters Thesis, University of Kansas. Accessed November 13, 2019. http://hdl.handle.net/1808/19593.

MLA Handbook (7th Edition):

Schueler, Samantha Katelyn. “A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions.” 2014. Web. 13 Nov 2019.

Vancouver:

Schueler SK. A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions. [Internet] [Masters thesis]. University of Kansas; 2014. [cited 2019 Nov 13]. Available from: http://hdl.handle.net/1808/19593.

Council of Science Editors:

Schueler SK. A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions. [Masters Thesis]. University of Kansas; 2014. Available from: http://hdl.handle.net/1808/19593


University of Manchester

3. Miller, Simon James. Adaptive wing structures for aeroelastic drag reduction and loads alleviation.

Degree: PhD, 2011, University of Manchester

 An investigation into two distinct novel adaptive structures concepts is performed with a view to improving the aerodynamic efficiency of aircraft wings.The main focus of… (more)

Subjects/Keywords: 629.13; Aeroelasticity; Aircraft morphing; Adaptive wing structures

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APA (6th Edition):

Miller, S. J. (2011). Adaptive wing structures for aeroelastic drag reduction and loads alleviation. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/adaptive-wing-structures-for-aeroelastic-drag-reduction-and-loadsalleviation(562181ed-7153-44cb-b0c7-9bfe1f79ae0f).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.542701

Chicago Manual of Style (16th Edition):

Miller, Simon James. “Adaptive wing structures for aeroelastic drag reduction and loads alleviation.” 2011. Doctoral Dissertation, University of Manchester. Accessed November 13, 2019. https://www.research.manchester.ac.uk/portal/en/theses/adaptive-wing-structures-for-aeroelastic-drag-reduction-and-loadsalleviation(562181ed-7153-44cb-b0c7-9bfe1f79ae0f).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.542701.

MLA Handbook (7th Edition):

Miller, Simon James. “Adaptive wing structures for aeroelastic drag reduction and loads alleviation.” 2011. Web. 13 Nov 2019.

Vancouver:

Miller SJ. Adaptive wing structures for aeroelastic drag reduction and loads alleviation. [Internet] [Doctoral dissertation]. University of Manchester; 2011. [cited 2019 Nov 13]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/adaptive-wing-structures-for-aeroelastic-drag-reduction-and-loadsalleviation(562181ed-7153-44cb-b0c7-9bfe1f79ae0f).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.542701.

Council of Science Editors:

Miller SJ. Adaptive wing structures for aeroelastic drag reduction and loads alleviation. [Doctoral Dissertation]. University of Manchester; 2011. Available from: https://www.research.manchester.ac.uk/portal/en/theses/adaptive-wing-structures-for-aeroelastic-drag-reduction-and-loadsalleviation(562181ed-7153-44cb-b0c7-9bfe1f79ae0f).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.542701


University of Manchester

4. Miller, Simon James. Adaptive wing structures for aeroelastic drag reduction and loadsalleviation.

Degree: 2011, University of Manchester

 An investigation into two distinct novel adaptive structures concepts is performed with a view to improving the aerodynamic efficiency of aircraft wings.The main focus of… (more)

Subjects/Keywords: Aeroelasticity; Aircraft morphing; Adaptive wing structures

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APA (6th Edition):

Miller, S. J. (2011). Adaptive wing structures for aeroelastic drag reduction and loadsalleviation. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:120148

Chicago Manual of Style (16th Edition):

Miller, Simon James. “Adaptive wing structures for aeroelastic drag reduction and loadsalleviation.” 2011. Doctoral Dissertation, University of Manchester. Accessed November 13, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:120148.

MLA Handbook (7th Edition):

Miller, Simon James. “Adaptive wing structures for aeroelastic drag reduction and loadsalleviation.” 2011. Web. 13 Nov 2019.

Vancouver:

Miller SJ. Adaptive wing structures for aeroelastic drag reduction and loadsalleviation. [Internet] [Doctoral dissertation]. University of Manchester; 2011. [cited 2019 Nov 13]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:120148.

Council of Science Editors:

Miller SJ. Adaptive wing structures for aeroelastic drag reduction and loadsalleviation. [Doctoral Dissertation]. University of Manchester; 2011. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:120148


North Carolina State University

5. Vosburg, Victor Jay. The Stability and Control of an Aircraft with an Adaptive Wing.

Degree: MS, Aerospace Engineering, 2005, North Carolina State University

 With increasing interest in the use of adaptive lifting surfaces for improved aircraft performance, it is necessary to study the stability and control characteristics of… (more)

Subjects/Keywords: AeroSim; Adaptive Wing; Stability and Control

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APA (6th Edition):

Vosburg, V. J. (2005). The Stability and Control of an Aircraft with an Adaptive Wing. (Thesis). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/1932

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Vosburg, Victor Jay. “The Stability and Control of an Aircraft with an Adaptive Wing.” 2005. Thesis, North Carolina State University. Accessed November 13, 2019. http://www.lib.ncsu.edu/resolver/1840.16/1932.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Vosburg, Victor Jay. “The Stability and Control of an Aircraft with an Adaptive Wing.” 2005. Web. 13 Nov 2019.

Vancouver:

Vosburg VJ. The Stability and Control of an Aircraft with an Adaptive Wing. [Internet] [Thesis]. North Carolina State University; 2005. [cited 2019 Nov 13]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/1932.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Vosburg VJ. The Stability and Control of an Aircraft with an Adaptive Wing. [Thesis]. North Carolina State University; 2005. Available from: http://www.lib.ncsu.edu/resolver/1840.16/1932

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Dayton

6. Puttmann, John Paul. Spatially Targeted Activation of a SMP.

Degree: MS(M.S.), Aerospace Engineering, 2018, University of Dayton

 The purpose of the research is to identify the mechanical properties of a skin, an infilled honeycomb, for morphing aircraft and investigate ways to optimize… (more)

Subjects/Keywords: Aerospace Engineering; SMP; Morphing Skin; adaptive structure; honeycomb; morphing wing; morphing skin; composite skin; aerospace structures; monolithic skin

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APA (6th Edition):

Puttmann, J. P. (2018). Spatially Targeted Activation of a SMP. (Masters Thesis). University of Dayton. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=dayton1525166147319011

Chicago Manual of Style (16th Edition):

Puttmann, John Paul. “Spatially Targeted Activation of a SMP.” 2018. Masters Thesis, University of Dayton. Accessed November 13, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1525166147319011.

MLA Handbook (7th Edition):

Puttmann, John Paul. “Spatially Targeted Activation of a SMP.” 2018. Web. 13 Nov 2019.

Vancouver:

Puttmann JP. Spatially Targeted Activation of a SMP. [Internet] [Masters thesis]. University of Dayton; 2018. [cited 2019 Nov 13]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1525166147319011.

Council of Science Editors:

Puttmann JP. Spatially Targeted Activation of a SMP. [Masters Thesis]. University of Dayton; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1525166147319011


North Carolina State University

7. King, Rachel Marie. On the Use of Wing Adaptation and Formation for Improved Aerodynamic Efficiency.

Degree: PhD, Aerospace Engineering, 2005, North Carolina State University

 There is a continuous effort to improve the performance and efficiency of today's aircraft, and the reduction of aircraft drag has been the primary focus… (more)

Subjects/Keywords: aerodynamic efficiency; adaptive wing; formation flight; ground-effect flight

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APA (6th Edition):

King, R. M. (2005). On the Use of Wing Adaptation and Formation for Improved Aerodynamic Efficiency. (Doctoral Dissertation). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/5759

Chicago Manual of Style (16th Edition):

King, Rachel Marie. “On the Use of Wing Adaptation and Formation for Improved Aerodynamic Efficiency.” 2005. Doctoral Dissertation, North Carolina State University. Accessed November 13, 2019. http://www.lib.ncsu.edu/resolver/1840.16/5759.

MLA Handbook (7th Edition):

King, Rachel Marie. “On the Use of Wing Adaptation and Formation for Improved Aerodynamic Efficiency.” 2005. Web. 13 Nov 2019.

Vancouver:

King RM. On the Use of Wing Adaptation and Formation for Improved Aerodynamic Efficiency. [Internet] [Doctoral dissertation]. North Carolina State University; 2005. [cited 2019 Nov 13]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/5759.

Council of Science Editors:

King RM. On the Use of Wing Adaptation and Formation for Improved Aerodynamic Efficiency. [Doctoral Dissertation]. North Carolina State University; 2005. Available from: http://www.lib.ncsu.edu/resolver/1840.16/5759


University of Waterloo

8. Koksal, Nasrettin. Adaptive and Optimal Motion Control of Multi-UAV Systems.

Degree: 2019, University of Waterloo

 This thesis studies trajectory tracking and coordination control problems for single and multi unmanned aerial vehicle (UAV) systems. These control problems are addressed for both… (more)

Subjects/Keywords: quadrotor UAV; fixed-wing UAV; adaptive linear quadratic tracking; least squares estimation; prescribed performance bound; backstepping control; formation control; adaptive mixing control

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APA (6th Edition):

Koksal, N. (2019). Adaptive and Optimal Motion Control of Multi-UAV Systems. (Thesis). University of Waterloo. Retrieved from http://hdl.handle.net/10012/14649

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Koksal, Nasrettin. “Adaptive and Optimal Motion Control of Multi-UAV Systems.” 2019. Thesis, University of Waterloo. Accessed November 13, 2019. http://hdl.handle.net/10012/14649.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Koksal, Nasrettin. “Adaptive and Optimal Motion Control of Multi-UAV Systems.” 2019. Web. 13 Nov 2019.

Vancouver:

Koksal N. Adaptive and Optimal Motion Control of Multi-UAV Systems. [Internet] [Thesis]. University of Waterloo; 2019. [cited 2019 Nov 13]. Available from: http://hdl.handle.net/10012/14649.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Koksal N. Adaptive and Optimal Motion Control of Multi-UAV Systems. [Thesis]. University of Waterloo; 2019. Available from: http://hdl.handle.net/10012/14649

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Alberta

9. Lumley, Lisa Margaret. Species delimitation in the Choristoneura fumiferana species complex (Lepidoptera: Tortricidae).

Degree: PhD, Department of Biological Sciences, 2010, University of Alberta

 Species identifications have been historically difficult in the economically important spruce budworm (Choristoneura fumiferana) pest complex. Morphological, ecological, behavioural, and genetic characters have been studied… (more)

Subjects/Keywords: neutral markers; phenology; species identification; microsatellites; Tortricidae; morphometrics; simple sequence repeats; Pheromones; wing colour; introgression; adaptive traits; mitochondrial DNA; species delimitation; speciation; Choristoneura; spruce budworm; Cypress Hills; Lepidoptera; hybridization

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APA (6th Edition):

Lumley, L. M. (2010). Species delimitation in the Choristoneura fumiferana species complex (Lepidoptera: Tortricidae). (Doctoral Dissertation). University of Alberta. Retrieved from https://era.library.ualberta.ca/files/0v838193j

Chicago Manual of Style (16th Edition):

Lumley, Lisa Margaret. “Species delimitation in the Choristoneura fumiferana species complex (Lepidoptera: Tortricidae).” 2010. Doctoral Dissertation, University of Alberta. Accessed November 13, 2019. https://era.library.ualberta.ca/files/0v838193j.

MLA Handbook (7th Edition):

Lumley, Lisa Margaret. “Species delimitation in the Choristoneura fumiferana species complex (Lepidoptera: Tortricidae).” 2010. Web. 13 Nov 2019.

Vancouver:

Lumley LM. Species delimitation in the Choristoneura fumiferana species complex (Lepidoptera: Tortricidae). [Internet] [Doctoral dissertation]. University of Alberta; 2010. [cited 2019 Nov 13]. Available from: https://era.library.ualberta.ca/files/0v838193j.

Council of Science Editors:

Lumley LM. Species delimitation in the Choristoneura fumiferana species complex (Lepidoptera: Tortricidae). [Doctoral Dissertation]. University of Alberta; 2010. Available from: https://era.library.ualberta.ca/files/0v838193j


North Carolina State University

10. Shipley, Edward Nicholas Jr. Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag.

Degree: MS, Aerospace Engineering, 2006, North Carolina State University

 This thesis presents a methodology to calculate the flap angles necessary to reproduce a desired lift distribution for an elastic wing with multiple trailing-edge flaps.… (more)

Subjects/Keywords: adaptive wing; elliptic lift; profile drag; induced drag; aerodynamics; aeroelasticity

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APA (6th Edition):

Shipley, E. N. J. (2006). Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag. (Thesis). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/1118

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Shipley, Edward Nicholas Jr. “Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag.” 2006. Thesis, North Carolina State University. Accessed November 13, 2019. http://www.lib.ncsu.edu/resolver/1840.16/1118.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Shipley, Edward Nicholas Jr. “Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag.” 2006. Web. 13 Nov 2019.

Vancouver:

Shipley ENJ. Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag. [Internet] [Thesis]. North Carolina State University; 2006. [cited 2019 Nov 13]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/1118.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Shipley ENJ. Static Aeroelasticity Considerations in Aerodynamic Adaptation of Wings for Low Drag. [Thesis]. North Carolina State University; 2006. Available from: http://www.lib.ncsu.edu/resolver/1840.16/1118

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Kentucky

11. Pern, Nan Jou. CHARACTERIZATION OF ZERO MASS FLUX FLOW CONTROL FOR LOW SPEED AIRFOIL SEPARATION CONTROL.

Degree: 2008, University of Kentucky

 An adaptive wing, a zero mass ux ow control device for low speed airfoil separation control, is investigated both experimentally and computationally at low speeds.… (more)

Subjects/Keywords: Adaptive Wing; Separation; Flow Control; Low Reynolds Number; Zero Mass Flux

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APA (6th Edition):

Pern, N. J. (2008). CHARACTERIZATION OF ZERO MASS FLUX FLOW CONTROL FOR LOW SPEED AIRFOIL SEPARATION CONTROL. (Doctoral Dissertation). University of Kentucky. Retrieved from https://uknowledge.uky.edu/gradschool_diss/577

Chicago Manual of Style (16th Edition):

Pern, Nan Jou. “CHARACTERIZATION OF ZERO MASS FLUX FLOW CONTROL FOR LOW SPEED AIRFOIL SEPARATION CONTROL.” 2008. Doctoral Dissertation, University of Kentucky. Accessed November 13, 2019. https://uknowledge.uky.edu/gradschool_diss/577.

MLA Handbook (7th Edition):

Pern, Nan Jou. “CHARACTERIZATION OF ZERO MASS FLUX FLOW CONTROL FOR LOW SPEED AIRFOIL SEPARATION CONTROL.” 2008. Web. 13 Nov 2019.

Vancouver:

Pern NJ. CHARACTERIZATION OF ZERO MASS FLUX FLOW CONTROL FOR LOW SPEED AIRFOIL SEPARATION CONTROL. [Internet] [Doctoral dissertation]. University of Kentucky; 2008. [cited 2019 Nov 13]. Available from: https://uknowledge.uky.edu/gradschool_diss/577.

Council of Science Editors:

Pern NJ. CHARACTERIZATION OF ZERO MASS FLUX FLOW CONTROL FOR LOW SPEED AIRFOIL SEPARATION CONTROL. [Doctoral Dissertation]. University of Kentucky; 2008. Available from: https://uknowledge.uky.edu/gradschool_diss/577


University of Florida

12. Wu, Pin. Experimental Characterization, Design, Analysis and Optimization of Flexible Flapping Wings for Micro Air Vehicles.

Degree: PhD, Mechanical Engineering - Mechanical and Aerospace Engineering, 2010, University of Florida

 This work has advanced the understanding of flapping flight of flexible wings designed to be used in micro air vehicles. A complete new experimental setup… (more)

Subjects/Keywords: Aerodynamics; Aircraft wings; Animal wings; Bending; Hovering; Insects; Kinematics; Leading edges; Stiffness; Structural deflection; adaptive, aeroelasticity, air, airflow, analysis, bioinspiration, correlation, deformation, dic, digital, experimental, flapping, flexible, flight, hummingbird, image, insect, mav, mechanism, micro, modal, nav, optical, passive, propulsion, vehicle, wing

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APA (6th Edition):

Wu, P. (2010). Experimental Characterization, Design, Analysis and Optimization of Flexible Flapping Wings for Micro Air Vehicles. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0041978

Chicago Manual of Style (16th Edition):

Wu, Pin. “Experimental Characterization, Design, Analysis and Optimization of Flexible Flapping Wings for Micro Air Vehicles.” 2010. Doctoral Dissertation, University of Florida. Accessed November 13, 2019. http://ufdc.ufl.edu/UFE0041978.

MLA Handbook (7th Edition):

Wu, Pin. “Experimental Characterization, Design, Analysis and Optimization of Flexible Flapping Wings for Micro Air Vehicles.” 2010. Web. 13 Nov 2019.

Vancouver:

Wu P. Experimental Characterization, Design, Analysis and Optimization of Flexible Flapping Wings for Micro Air Vehicles. [Internet] [Doctoral dissertation]. University of Florida; 2010. [cited 2019 Nov 13]. Available from: http://ufdc.ufl.edu/UFE0041978.

Council of Science Editors:

Wu P. Experimental Characterization, Design, Analysis and Optimization of Flexible Flapping Wings for Micro Air Vehicles. [Doctoral Dissertation]. University of Florida; 2010. Available from: http://ufdc.ufl.edu/UFE0041978


University of New South Wales

13. Samal, Mahendra. Neural network based identification and control of an unmanned helicopter.

Degree: Engineering & Information Technology, 2009, University of New South Wales

 This research work provides the development of an Adaptive Flight Control System (AFCS) for autonomous hover of a Rotary-wing Unmanned Aerial Vehicle (RUAV). Due to… (more)

Subjects/Keywords: Model Predictive Control (MPC); Adaptive Flight Control System; Rotary-wing Unmanned Aerial Vehicle (RUAV); Auto-regressive neural network architecture; non-linear complex dynamic systems; Drone aircraft

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APA (6th Edition):

Samal, M. (2009). Neural network based identification and control of an unmanned helicopter. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/43917 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:7346/SOURCE01?view=true

Chicago Manual of Style (16th Edition):

Samal, Mahendra. “Neural network based identification and control of an unmanned helicopter.” 2009. Doctoral Dissertation, University of New South Wales. Accessed November 13, 2019. http://handle.unsw.edu.au/1959.4/43917 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:7346/SOURCE01?view=true.

MLA Handbook (7th Edition):

Samal, Mahendra. “Neural network based identification and control of an unmanned helicopter.” 2009. Web. 13 Nov 2019.

Vancouver:

Samal M. Neural network based identification and control of an unmanned helicopter. [Internet] [Doctoral dissertation]. University of New South Wales; 2009. [cited 2019 Nov 13]. Available from: http://handle.unsw.edu.au/1959.4/43917 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:7346/SOURCE01?view=true.

Council of Science Editors:

Samal M. Neural network based identification and control of an unmanned helicopter. [Doctoral Dissertation]. University of New South Wales; 2009. Available from: http://handle.unsw.edu.au/1959.4/43917 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:7346/SOURCE01?view=true


ETH Zürich

14. Quack, Manfred. Closed-Loop Control of Spanwise Lift Distribution for Morphing Wing Applications.

Degree: 2014, ETH Zürich

Subjects/Keywords: ADAPTIVE STRUKTUREN (INGENIEURWESEN); COMPUTATIONAL FLUID DYNAMICS (FLUIDMECHANIK); TRAGFLĂ„CHENSCHNITTE, PROFILE (AERODYNAMIK); PIEZOELECTRIC MATERIALS (ELECTRICAL ENGINEERING); COMPUTATIONAL FLUID DYNAMICS (FLUID MECHANICS); WING SECTIONS (AERODYNAMICS); ADAPTIVE STRUCTURES (ENGINEERING); PIEZOELEKTRISCHE WERKSTOFFE (ELEKTROTECHNIK); info:eu-repo/classification/ddc/620; Engineering & allied operations

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APA (6th Edition):

Quack, M. (2014). Closed-Loop Control of Spanwise Lift Distribution for Morphing Wing Applications. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/99167

Chicago Manual of Style (16th Edition):

Quack, Manfred. “Closed-Loop Control of Spanwise Lift Distribution for Morphing Wing Applications.” 2014. Doctoral Dissertation, ETH Zürich. Accessed November 13, 2019. http://hdl.handle.net/20.500.11850/99167.

MLA Handbook (7th Edition):

Quack, Manfred. “Closed-Loop Control of Spanwise Lift Distribution for Morphing Wing Applications.” 2014. Web. 13 Nov 2019.

Vancouver:

Quack M. Closed-Loop Control of Spanwise Lift Distribution for Morphing Wing Applications. [Internet] [Doctoral dissertation]. ETH Zürich; 2014. [cited 2019 Nov 13]. Available from: http://hdl.handle.net/20.500.11850/99167.

Council of Science Editors:

Quack M. Closed-Loop Control of Spanwise Lift Distribution for Morphing Wing Applications. [Doctoral Dissertation]. ETH Zürich; 2014. Available from: http://hdl.handle.net/20.500.11850/99167

15. Marchini, Brian Decimo. Adaptive Control Techniques for Transition-to-Hover Flight of Fixed-Wing UAVs.

Degree: MS, Aerospace Engineering, 2013, Cal Poly

  Fixed-wing unmanned aerial vehicles (UAVs) with the ability to hover combine the speed and endurance of traditional fixed-wing fight with the stable hovering and… (more)

Subjects/Keywords: Unmanned Aerial Vehicles; Adaptive Control; Autopilots; Arduino; ArduPilot; Fixed-Wing Hovering; Aerodynamics and Fluid Mechanics; Aeronautical Vehicles; Navigation, Guidance, Control and Dynamics

…37 4.4 Simple Nonlinear Model Reference Adaptive Controller . . . . . . . . 39 4.5… …ADAPTIVE simulation results (rise time = 3 sec, approach speed = 60 ft/sec, wind speed = 10… …HOVER ADAPTIVE simulation results (rise time = 1 sec, approach speed = 60 ft/sec, wind… …93 6.17 MRAC Simulation Results: HOVER ADAPTIVE simulations showed the same linear… …117 7.9 MRAC Flight Test Example: HOVER ADAPTIVE flight results with approach peed = 60 ft… 

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Marchini, B. D. (2013). Adaptive Control Techniques for Transition-to-Hover Flight of Fixed-Wing UAVs. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1108 ; 10.15368/theses.2013.191

Chicago Manual of Style (16th Edition):

Marchini, Brian Decimo. “Adaptive Control Techniques for Transition-to-Hover Flight of Fixed-Wing UAVs.” 2013. Masters Thesis, Cal Poly. Accessed November 13, 2019. https://digitalcommons.calpoly.edu/theses/1108 ; 10.15368/theses.2013.191.

MLA Handbook (7th Edition):

Marchini, Brian Decimo. “Adaptive Control Techniques for Transition-to-Hover Flight of Fixed-Wing UAVs.” 2013. Web. 13 Nov 2019.

Vancouver:

Marchini BD. Adaptive Control Techniques for Transition-to-Hover Flight of Fixed-Wing UAVs. [Internet] [Masters thesis]. Cal Poly; 2013. [cited 2019 Nov 13]. Available from: https://digitalcommons.calpoly.edu/theses/1108 ; 10.15368/theses.2013.191.

Council of Science Editors:

Marchini BD. Adaptive Control Techniques for Transition-to-Hover Flight of Fixed-Wing UAVs. [Masters Thesis]. Cal Poly; 2013. Available from: https://digitalcommons.calpoly.edu/theses/1108 ; 10.15368/theses.2013.191

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