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You searched for subject:(Micro Air Vehicle). Showing records 1 – 30 of 71 total matches.

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Anna University

1. Muniappan, A. Design and development of flapping wing micro air vehicle; -.

Degree: Mechanical Engineering, 2014, Anna University

Recent advances in microtechnology have created an opportunity newlineto mount miniature surveillance equipment on small flying aircraft known as newlineMicro Air Vehicles MAVs Such microtechnology… (more)

Subjects/Keywords: flapping wing; mechanical engineering; micro air vehicle

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APA (6th Edition):

Muniappan, A. (2014). Design and development of flapping wing micro air vehicle; -. (Thesis). Anna University. Retrieved from http://shodhganga.inflibnet.ac.in/handle/10603/27367

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):

Muniappan, A. “Design and development of flapping wing micro air vehicle; -.” 2014. Thesis, Anna University. Accessed January 23, 2021. http://shodhganga.inflibnet.ac.in/handle/10603/27367.

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

MLA Handbook (7th Edition):

Muniappan, A. “Design and development of flapping wing micro air vehicle; -.” 2014. Web. 23 Jan 2021.

Vancouver:

Muniappan A. Design and development of flapping wing micro air vehicle; -. [Internet] [Thesis]. Anna University; 2014. [cited 2021 Jan 23]. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/27367.

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

Council of Science Editors:

Muniappan A. Design and development of flapping wing micro air vehicle; -. [Thesis]. Anna University; 2014. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/27367

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


Delft University of Technology

2. Peters, H.J. (author). The Optimization of the Flapping Wings for a Micro Air Vehicle.

Degree: 2011, Delft University of Technology

Precision and Microsystems Engineering

Mechanical, Maritime and Materials Engineering

Advisors/Committee Members: Goosen, J.F.L. (mentor).

Subjects/Keywords: Micro Air Vehicle

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APA (6th Edition):

Peters, H. J. (. (2011). The Optimization of the Flapping Wings for a Micro Air Vehicle. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f42d9d82-ed7f-450d-9c5b-7d34d3ae2725

Chicago Manual of Style (16th Edition):

Peters, H J (author). “The Optimization of the Flapping Wings for a Micro Air Vehicle.” 2011. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:f42d9d82-ed7f-450d-9c5b-7d34d3ae2725.

MLA Handbook (7th Edition):

Peters, H J (author). “The Optimization of the Flapping Wings for a Micro Air Vehicle.” 2011. Web. 23 Jan 2021.

Vancouver:

Peters HJ(. The Optimization of the Flapping Wings for a Micro Air Vehicle. [Internet] [Masters thesis]. Delft University of Technology; 2011. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:f42d9d82-ed7f-450d-9c5b-7d34d3ae2725.

Council of Science Editors:

Peters HJ(. The Optimization of the Flapping Wings for a Micro Air Vehicle. [Masters Thesis]. Delft University of Technology; 2011. Available from: http://resolver.tudelft.nl/uuid:f42d9d82-ed7f-450d-9c5b-7d34d3ae2725


Rochester Institute of Technology

3. Prosser, Daniel. Flapping wing design for a dragonfly-like micro air vehicle.

Degree: Mechanical Engineering, 2011, Rochester Institute of Technology

 In this thesis, the aerodynamics of the Quad-Wing Vehicle, a Micro Air Vehicle designed to hover with four flapping wings in a dragonfly-like configuration, is… (more)

Subjects/Keywords: Bio-inspired; CFD; Computational fluid dynamics; Flapping; MAV; Micro air vehicle

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APA (6th Edition):

Prosser, D. (2011). Flapping wing design for a dragonfly-like micro air vehicle. (Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/5804

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):

Prosser, Daniel. “Flapping wing design for a dragonfly-like micro air vehicle.” 2011. Thesis, Rochester Institute of Technology. Accessed January 23, 2021. https://scholarworks.rit.edu/theses/5804.

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

MLA Handbook (7th Edition):

Prosser, Daniel. “Flapping wing design for a dragonfly-like micro air vehicle.” 2011. Web. 23 Jan 2021.

Vancouver:

Prosser D. Flapping wing design for a dragonfly-like micro air vehicle. [Internet] [Thesis]. Rochester Institute of Technology; 2011. [cited 2021 Jan 23]. Available from: https://scholarworks.rit.edu/theses/5804.

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

Council of Science Editors:

Prosser D. Flapping wing design for a dragonfly-like micro air vehicle. [Thesis]. Rochester Institute of Technology; 2011. Available from: https://scholarworks.rit.edu/theses/5804

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


Harvard University

4. Finio, Benjamin. Roll, Pitch and Yaw Torque Control for a Robotic Bee.

Degree: PhD, Engineering Sciences, 2012, Harvard University

In the last decade, the robotics community has pushed to develop increasingly small, autonomous flapping-wing robotic vehicles for a variety of civilian and military applications.… (more)

Subjects/Keywords: MAV; robotic insect; robotics; mechanical engineering; engineering; micro air vehicle; robobee

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APA (6th Edition):

Finio, B. (2012). Roll, Pitch and Yaw Torque Control for a Robotic Bee. (Doctoral Dissertation). Harvard University. Retrieved from http://nrs.harvard.edu/urn-3:HUL.InstRepos:9920663

Chicago Manual of Style (16th Edition):

Finio, Benjamin. “Roll, Pitch and Yaw Torque Control for a Robotic Bee.” 2012. Doctoral Dissertation, Harvard University. Accessed January 23, 2021. http://nrs.harvard.edu/urn-3:HUL.InstRepos:9920663.

MLA Handbook (7th Edition):

Finio, Benjamin. “Roll, Pitch and Yaw Torque Control for a Robotic Bee.” 2012. Web. 23 Jan 2021.

Vancouver:

Finio B. Roll, Pitch and Yaw Torque Control for a Robotic Bee. [Internet] [Doctoral dissertation]. Harvard University; 2012. [cited 2021 Jan 23]. Available from: http://nrs.harvard.edu/urn-3:HUL.InstRepos:9920663.

Council of Science Editors:

Finio B. Roll, Pitch and Yaw Torque Control for a Robotic Bee. [Doctoral Dissertation]. Harvard University; 2012. Available from: http://nrs.harvard.edu/urn-3:HUL.InstRepos:9920663

5. Van den Heuvel, H.N. (author). Conceptual Development of a Catalytic Expansion Actuator for a Resonating-body Flapping-wing Micro Air Vehicle.

Degree: 2015, Delft University of Technology

In this project a start has been made in the conceptual and practical development of a hydrogen peroxide catalytic micro expansion engine. The liquid fuel… (more)

Subjects/Keywords: Catalytic Expansion Actuator; Resonating-body; Flapping-wing; Micro Air Vehicle

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APA (6th Edition):

Van den Heuvel, H. N. (. (2015). Conceptual Development of a Catalytic Expansion Actuator for a Resonating-body Flapping-wing Micro Air Vehicle. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f4a04b1a-fbb8-4855-a613-993713aece7c

Chicago Manual of Style (16th Edition):

Van den Heuvel, H N (author). “Conceptual Development of a Catalytic Expansion Actuator for a Resonating-body Flapping-wing Micro Air Vehicle.” 2015. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:f4a04b1a-fbb8-4855-a613-993713aece7c.

MLA Handbook (7th Edition):

Van den Heuvel, H N (author). “Conceptual Development of a Catalytic Expansion Actuator for a Resonating-body Flapping-wing Micro Air Vehicle.” 2015. Web. 23 Jan 2021.

Vancouver:

Van den Heuvel HN(. Conceptual Development of a Catalytic Expansion Actuator for a Resonating-body Flapping-wing Micro Air Vehicle. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:f4a04b1a-fbb8-4855-a613-993713aece7c.

Council of Science Editors:

Van den Heuvel HN(. Conceptual Development of a Catalytic Expansion Actuator for a Resonating-body Flapping-wing Micro Air Vehicle. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:f4a04b1a-fbb8-4855-a613-993713aece7c


RMIT University

6. Fisher, A. The effect of freestream turbulence on fixed and flapping micro air vehicle wings.

Degree: 2013, RMIT University

 This thesis details an experimental investigation into the effects of elevated levels of large-scale freestream turbulence on the aerodynamics of a micro air vehicle wing… (more)

Subjects/Keywords: Fields of Research; micro air vehicle; MAV; flapping; aerodynamics; pressure measurement; atmospheric turbulence

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APA (6th Edition):

Fisher, A. (2013). The effect of freestream turbulence on fixed and flapping micro air vehicle wings. (Thesis). RMIT University. Retrieved from http://researchbank.rmit.edu.au/view/rmit:160502

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):

Fisher, A. “The effect of freestream turbulence on fixed and flapping micro air vehicle wings.” 2013. Thesis, RMIT University. Accessed January 23, 2021. http://researchbank.rmit.edu.au/view/rmit:160502.

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

MLA Handbook (7th Edition):

Fisher, A. “The effect of freestream turbulence on fixed and flapping micro air vehicle wings.” 2013. Web. 23 Jan 2021.

Vancouver:

Fisher A. The effect of freestream turbulence on fixed and flapping micro air vehicle wings. [Internet] [Thesis]. RMIT University; 2013. [cited 2021 Jan 23]. Available from: http://researchbank.rmit.edu.au/view/rmit:160502.

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

Council of Science Editors:

Fisher A. The effect of freestream turbulence on fixed and flapping micro air vehicle wings. [Thesis]. RMIT University; 2013. Available from: http://researchbank.rmit.edu.au/view/rmit:160502

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


RMIT University

7. Mohamed, A. Phase-advanced attitude sensing and control for fixed-wing micro aerial vehicles in turbulence.

Degree: 2015, RMIT University

 The scale of fixed-wing Micro Aerial Vehicles (MAVs) lend them to many unique applications. These applications often require low speed flights close to the ground,… (more)

Subjects/Keywords: Fields of Research; Attitude Control; Turbulence; Bio-inspired; Micro Air Vehicle; Phase advanced sensing

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APA (6th Edition):

Mohamed, A. (2015). Phase-advanced attitude sensing and control for fixed-wing micro aerial vehicles in turbulence. (Thesis). RMIT University. Retrieved from http://researchbank.rmit.edu.au/view/rmit:162425

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):

Mohamed, A. “Phase-advanced attitude sensing and control for fixed-wing micro aerial vehicles in turbulence.” 2015. Thesis, RMIT University. Accessed January 23, 2021. http://researchbank.rmit.edu.au/view/rmit:162425.

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

MLA Handbook (7th Edition):

Mohamed, A. “Phase-advanced attitude sensing and control for fixed-wing micro aerial vehicles in turbulence.” 2015. Web. 23 Jan 2021.

Vancouver:

Mohamed A. Phase-advanced attitude sensing and control for fixed-wing micro aerial vehicles in turbulence. [Internet] [Thesis]. RMIT University; 2015. [cited 2021 Jan 23]. Available from: http://researchbank.rmit.edu.au/view/rmit:162425.

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

Council of Science Editors:

Mohamed A. Phase-advanced attitude sensing and control for fixed-wing micro aerial vehicles in turbulence. [Thesis]. RMIT University; 2015. Available from: http://researchbank.rmit.edu.au/view/rmit:162425

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


Delft University of Technology

8. Deng, S. Aerodynamics of flapping-wing Micro-Air-Vehicle: An integrated experimental and numerical study.

Degree: 2016, Delft University of Technology

 The interest in Micro Air Vehicles (MAVs) has stimulated continuous research activities, in view of their potential in civilian and military applications. An autonomous MAV… (more)

Subjects/Keywords: flapping wing; Micro Air Vehicle; aerodynamics

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APA (6th Edition):

Deng, S. (2016). Aerodynamics of flapping-wing Micro-Air-Vehicle: An integrated experimental and numerical study. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:b1abe278-bb42-481b-bc5b-7af53424bc75 ; urn:NBN:nl:ui:24-uuid:b1abe278-bb42-481b-bc5b-7af53424bc75 ; urn:NBN:nl:ui:24-uuid:b1abe278-bb42-481b-bc5b-7af53424bc75 ; http://resolver.tudelft.nl/uuid:b1abe278-bb42-481b-bc5b-7af53424bc75

Chicago Manual of Style (16th Edition):

Deng, S. “Aerodynamics of flapping-wing Micro-Air-Vehicle: An integrated experimental and numerical study.” 2016. Doctoral Dissertation, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:b1abe278-bb42-481b-bc5b-7af53424bc75 ; urn:NBN:nl:ui:24-uuid:b1abe278-bb42-481b-bc5b-7af53424bc75 ; urn:NBN:nl:ui:24-uuid:b1abe278-bb42-481b-bc5b-7af53424bc75 ; http://resolver.tudelft.nl/uuid:b1abe278-bb42-481b-bc5b-7af53424bc75.

MLA Handbook (7th Edition):

Deng, S. “Aerodynamics of flapping-wing Micro-Air-Vehicle: An integrated experimental and numerical study.” 2016. Web. 23 Jan 2021.

Vancouver:

Deng S. Aerodynamics of flapping-wing Micro-Air-Vehicle: An integrated experimental and numerical study. [Internet] [Doctoral dissertation]. Delft University of Technology; 2016. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:b1abe278-bb42-481b-bc5b-7af53424bc75 ; urn:NBN:nl:ui:24-uuid:b1abe278-bb42-481b-bc5b-7af53424bc75 ; urn:NBN:nl:ui:24-uuid:b1abe278-bb42-481b-bc5b-7af53424bc75 ; http://resolver.tudelft.nl/uuid:b1abe278-bb42-481b-bc5b-7af53424bc75.

Council of Science Editors:

Deng S. Aerodynamics of flapping-wing Micro-Air-Vehicle: An integrated experimental and numerical study. [Doctoral Dissertation]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:b1abe278-bb42-481b-bc5b-7af53424bc75 ; urn:NBN:nl:ui:24-uuid:b1abe278-bb42-481b-bc5b-7af53424bc75 ; urn:NBN:nl:ui:24-uuid:b1abe278-bb42-481b-bc5b-7af53424bc75 ; http://resolver.tudelft.nl/uuid:b1abe278-bb42-481b-bc5b-7af53424bc75


University of Maryland

9. Winslow, Justin Michael. UNDERSTANDING OF LOW REYNOLDS NUMBER AERODYNAMICS AND DESIGN OF MICRO ROTARY-WING AIR VEHICLES.

Degree: Aerospace Engineering, 2016, University of Maryland

 The goal of the present research is to understand aerodynamics at low Reynolds numbers and synthesize rules towards the development of hovering micro rotary-wing air(more)

Subjects/Keywords: Aerospace engineering; Design; Endurance; Low Reynolds Number; Micro Air Vehicle; Quadcopter; Quadrotor

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APA (6th Edition):

Winslow, J. M. (2016). UNDERSTANDING OF LOW REYNOLDS NUMBER AERODYNAMICS AND DESIGN OF MICRO ROTARY-WING AIR VEHICLES. (Thesis). University of Maryland. Retrieved from http://hdl.handle.net/1903/19319

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):

Winslow, Justin Michael. “UNDERSTANDING OF LOW REYNOLDS NUMBER AERODYNAMICS AND DESIGN OF MICRO ROTARY-WING AIR VEHICLES.” 2016. Thesis, University of Maryland. Accessed January 23, 2021. http://hdl.handle.net/1903/19319.

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

MLA Handbook (7th Edition):

Winslow, Justin Michael. “UNDERSTANDING OF LOW REYNOLDS NUMBER AERODYNAMICS AND DESIGN OF MICRO ROTARY-WING AIR VEHICLES.” 2016. Web. 23 Jan 2021.

Vancouver:

Winslow JM. UNDERSTANDING OF LOW REYNOLDS NUMBER AERODYNAMICS AND DESIGN OF MICRO ROTARY-WING AIR VEHICLES. [Internet] [Thesis]. University of Maryland; 2016. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/1903/19319.

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

Council of Science Editors:

Winslow JM. UNDERSTANDING OF LOW REYNOLDS NUMBER AERODYNAMICS AND DESIGN OF MICRO ROTARY-WING AIR VEHICLES. [Thesis]. University of Maryland; 2016. Available from: http://hdl.handle.net/1903/19319

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


University of Maryland

10. Gerardi, Steven Anthony. An Observer for Estimating Translational Velocity from Optic Flow and Radar.

Degree: Aerospace Engineering, 2011, University of Maryland

 This thesis presents the development of a discrete time observer for estimating state information from optic flow and radar measurements. It is shown that estimates… (more)

Subjects/Keywords: Aerospace engineering; Autonomous; Micro Air Vehicle; Optic Flow; State Estimation; Vision-based Control

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APA (6th Edition):

Gerardi, S. A. (2011). An Observer for Estimating Translational Velocity from Optic Flow and Radar. (Thesis). University of Maryland. Retrieved from http://hdl.handle.net/1903/12220

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):

Gerardi, Steven Anthony. “An Observer for Estimating Translational Velocity from Optic Flow and Radar.” 2011. Thesis, University of Maryland. Accessed January 23, 2021. http://hdl.handle.net/1903/12220.

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

MLA Handbook (7th Edition):

Gerardi, Steven Anthony. “An Observer for Estimating Translational Velocity from Optic Flow and Radar.” 2011. Web. 23 Jan 2021.

Vancouver:

Gerardi SA. An Observer for Estimating Translational Velocity from Optic Flow and Radar. [Internet] [Thesis]. University of Maryland; 2011. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/1903/12220.

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

Council of Science Editors:

Gerardi SA. An Observer for Estimating Translational Velocity from Optic Flow and Radar. [Thesis]. University of Maryland; 2011. Available from: http://hdl.handle.net/1903/12220

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


Virginia Tech

11. Ohanian, Osgar John. Ducted Fan Aerodynamics and Modeling, with Applications of Steady and Synthetic Jet Flow Control.

Degree: PhD, Mechanical Engineering, 2011, Virginia Tech

 Ducted fan vehicles possess a superior ability to maximize payload capacity while minimizing vehicle size. Their ability to both hover and fly at high speed… (more)

Subjects/Keywords: non-dimensional; micro air vehicle; UAV; MAV; unmanned aerial vehicle; aerodynamic modeling; flow control; synthetic jets; rotor; shrouded propeller; ducted fan

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

APA (6th Edition):

Ohanian, O. J. (2011). Ducted Fan Aerodynamics and Modeling, with Applications of Steady and Synthetic Jet Flow Control. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/27687

Chicago Manual of Style (16th Edition):

Ohanian, Osgar John. “Ducted Fan Aerodynamics and Modeling, with Applications of Steady and Synthetic Jet Flow Control.” 2011. Doctoral Dissertation, Virginia Tech. Accessed January 23, 2021. http://hdl.handle.net/10919/27687.

MLA Handbook (7th Edition):

Ohanian, Osgar John. “Ducted Fan Aerodynamics and Modeling, with Applications of Steady and Synthetic Jet Flow Control.” 2011. Web. 23 Jan 2021.

Vancouver:

Ohanian OJ. Ducted Fan Aerodynamics and Modeling, with Applications of Steady and Synthetic Jet Flow Control. [Internet] [Doctoral dissertation]. Virginia Tech; 2011. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/10919/27687.

Council of Science Editors:

Ohanian OJ. Ducted Fan Aerodynamics and Modeling, with Applications of Steady and Synthetic Jet Flow Control. [Doctoral Dissertation]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/27687


University of Johannesburg

12. Cronje, Jaco. Binary image features designed towards vision-based localization and environment mapping from micro aerial vehicle (MAV) captured images.

Degree: 2012, University of Johannesburg

M.Phil.

This work proposes a fast local image feature detector and descriptor that is im- plementable on a GPU. The BFROST feature detector is the… (more)

Subjects/Keywords: Binary image; Micro aerial vehicle captured images; Remote sensing - Data processing; Micro air vehicles; Mobile geographic information systems; Imaging systems

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

APA (6th Edition):

Cronje, J. (2012). Binary image features designed towards vision-based localization and environment mapping from micro aerial vehicle (MAV) captured images. (Thesis). University of Johannesburg. Retrieved from http://hdl.handle.net/10210/7881

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):

Cronje, Jaco. “Binary image features designed towards vision-based localization and environment mapping from micro aerial vehicle (MAV) captured images.” 2012. Thesis, University of Johannesburg. Accessed January 23, 2021. http://hdl.handle.net/10210/7881.

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

MLA Handbook (7th Edition):

Cronje, Jaco. “Binary image features designed towards vision-based localization and environment mapping from micro aerial vehicle (MAV) captured images.” 2012. Web. 23 Jan 2021.

Vancouver:

Cronje J. Binary image features designed towards vision-based localization and environment mapping from micro aerial vehicle (MAV) captured images. [Internet] [Thesis]. University of Johannesburg; 2012. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/10210/7881.

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

Council of Science Editors:

Cronje J. Binary image features designed towards vision-based localization and environment mapping from micro aerial vehicle (MAV) captured images. [Thesis]. University of Johannesburg; 2012. Available from: http://hdl.handle.net/10210/7881

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


Virginia Tech

13. Evans, Richard Blaine. Modeling and Testing of a Micro-Tubular Low-Temperature Fuel Cell for use in a Micro Air Vehicle.

Degree: MS, Mechanical Engineering, 2007, Virginia Tech

Micro air vehicles (MAVs) are small remote controlled aircraft used by military personnel for reconnaissance and are currently powered by batteries. The MAVs rely on… (more)

Subjects/Keywords: PEM Fuel Cell; Micro-tubular; Micro Air Vehicle

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APA (6th Edition):

Evans, R. B. (2007). Modeling and Testing of a Micro-Tubular Low-Temperature Fuel Cell for use in a Micro Air Vehicle. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/36497

Chicago Manual of Style (16th Edition):

Evans, Richard Blaine. “Modeling and Testing of a Micro-Tubular Low-Temperature Fuel Cell for use in a Micro Air Vehicle.” 2007. Masters Thesis, Virginia Tech. Accessed January 23, 2021. http://hdl.handle.net/10919/36497.

MLA Handbook (7th Edition):

Evans, Richard Blaine. “Modeling and Testing of a Micro-Tubular Low-Temperature Fuel Cell for use in a Micro Air Vehicle.” 2007. Web. 23 Jan 2021.

Vancouver:

Evans RB. Modeling and Testing of a Micro-Tubular Low-Temperature Fuel Cell for use in a Micro Air Vehicle. [Internet] [Masters thesis]. Virginia Tech; 2007. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/10919/36497.

Council of Science Editors:

Evans RB. Modeling and Testing of a Micro-Tubular Low-Temperature Fuel Cell for use in a Micro Air Vehicle. [Masters Thesis]. Virginia Tech; 2007. Available from: http://hdl.handle.net/10919/36497

14. Doan, Le Anh. Du micro véhicule aérien au nano véhicule aérien : études théoriques et expérimentales sur un insecte artificiel à ailes battantes : Micro air vehicle to nano air vehicle : theoretical and experimental studies of an artificial flapping insect.

Degree: Docteur es, Électronique. Micro et nano technologie, 2019, Valenciennes

Au cours des dernières décennies, la possibilité d’exploiter les capacités de vol exceptionnelles des insectes a été à l’origine de nombreuses recherches sur l’élaboration de… (more)

Subjects/Keywords: Nano-Véhicules aérien; Micro-Véhicule aérien; Ailes battantes; Puissance; Énergie; Bond Graph; Nano air vehicles; Micro air vehicle; Flapping-Wing; Power; Energy

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APA (6th Edition):

Doan, L. A. (2019). Du micro véhicule aérien au nano véhicule aérien : études théoriques et expérimentales sur un insecte artificiel à ailes battantes : Micro air vehicle to nano air vehicle : theoretical and experimental studies of an artificial flapping insect. (Doctoral Dissertation). Valenciennes. Retrieved from http://www.theses.fr/2019VALE0004

Chicago Manual of Style (16th Edition):

Doan, Le Anh. “Du micro véhicule aérien au nano véhicule aérien : études théoriques et expérimentales sur un insecte artificiel à ailes battantes : Micro air vehicle to nano air vehicle : theoretical and experimental studies of an artificial flapping insect.” 2019. Doctoral Dissertation, Valenciennes. Accessed January 23, 2021. http://www.theses.fr/2019VALE0004.

MLA Handbook (7th Edition):

Doan, Le Anh. “Du micro véhicule aérien au nano véhicule aérien : études théoriques et expérimentales sur un insecte artificiel à ailes battantes : Micro air vehicle to nano air vehicle : theoretical and experimental studies of an artificial flapping insect.” 2019. Web. 23 Jan 2021.

Vancouver:

Doan LA. Du micro véhicule aérien au nano véhicule aérien : études théoriques et expérimentales sur un insecte artificiel à ailes battantes : Micro air vehicle to nano air vehicle : theoretical and experimental studies of an artificial flapping insect. [Internet] [Doctoral dissertation]. Valenciennes; 2019. [cited 2021 Jan 23]. Available from: http://www.theses.fr/2019VALE0004.

Council of Science Editors:

Doan LA. Du micro véhicule aérien au nano véhicule aérien : études théoriques et expérimentales sur un insecte artificiel à ailes battantes : Micro air vehicle to nano air vehicle : theoretical and experimental studies of an artificial flapping insect. [Doctoral Dissertation]. Valenciennes; 2019. Available from: http://www.theses.fr/2019VALE0004


Indian Institute of Science

15. Satak, Neha. Design, Development And Flight Control Of Sapthami - A Fixed Wing Micro Air Vehicle.

Degree: MSc Engg, Faculty of Engineering, 2010, Indian Institute of Science

 Two micro air vehicles, namely Sapthami and Sapthami-flyer, are developed in this thesis. Their total weight is less than 200grams each. They fit inside a… (more)

Subjects/Keywords: Flight Dynamics; Air Vehicle - Flight Dynamics; Sapthami (Air Vehicle); Micro Air Vehicle - Mathematical Model; Sapthami-flyer; Micro Air Vehicle (MAV); Iterative Linear Matrix Inequality Algorithm (ILMI); Aeronautics

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APA (6th Edition):

Satak, N. (2010). Design, Development And Flight Control Of Sapthami - A Fixed Wing Micro Air Vehicle. (Masters Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/872

Chicago Manual of Style (16th Edition):

Satak, Neha. “Design, Development And Flight Control Of Sapthami - A Fixed Wing Micro Air Vehicle.” 2010. Masters Thesis, Indian Institute of Science. Accessed January 23, 2021. http://etd.iisc.ac.in/handle/2005/872.

MLA Handbook (7th Edition):

Satak, Neha. “Design, Development And Flight Control Of Sapthami - A Fixed Wing Micro Air Vehicle.” 2010. Web. 23 Jan 2021.

Vancouver:

Satak N. Design, Development And Flight Control Of Sapthami - A Fixed Wing Micro Air Vehicle. [Internet] [Masters thesis]. Indian Institute of Science; 2010. [cited 2021 Jan 23]. Available from: http://etd.iisc.ac.in/handle/2005/872.

Council of Science Editors:

Satak N. Design, Development And Flight Control Of Sapthami - A Fixed Wing Micro Air Vehicle. [Masters Thesis]. Indian Institute of Science; 2010. Available from: http://etd.iisc.ac.in/handle/2005/872


RMIT University

16. Marino, M. Unsteady pressure sensing on a MAV wing for control inputs in turbulence.

Degree: 2013, RMIT University

 This thesis presents the results of systematic studies in which the effects of turbulence and how it impacts the aerodynamic performance of a Micro Air(more)

Subjects/Keywords: Fields of Research; micro air vehicle; MAV; wing; aerodynamics; pressure; sensing; control; atmospheric; turbulence; unsteady; control; stability

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APA (6th Edition):

Marino, M. (2013). Unsteady pressure sensing on a MAV wing for control inputs in turbulence. (Thesis). RMIT University. Retrieved from http://researchbank.rmit.edu.au/view/rmit:160572

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):

Marino, M. “Unsteady pressure sensing on a MAV wing for control inputs in turbulence.” 2013. Thesis, RMIT University. Accessed January 23, 2021. http://researchbank.rmit.edu.au/view/rmit:160572.

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

MLA Handbook (7th Edition):

Marino, M. “Unsteady pressure sensing on a MAV wing for control inputs in turbulence.” 2013. Web. 23 Jan 2021.

Vancouver:

Marino M. Unsteady pressure sensing on a MAV wing for control inputs in turbulence. [Internet] [Thesis]. RMIT University; 2013. [cited 2021 Jan 23]. Available from: http://researchbank.rmit.edu.au/view/rmit:160572.

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

Council of Science Editors:

Marino M. Unsteady pressure sensing on a MAV wing for control inputs in turbulence. [Thesis]. RMIT University; 2013. Available from: http://researchbank.rmit.edu.au/view/rmit:160572

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


Rochester Institute of Technology

17. Reid, Michael. Thin/cambered/reflexed airfoil development for micro-air vehicles at Reynolds numbers of 60,000 to 150,000.

Degree: Mechanical Engineering, 2006, Rochester Institute of Technology

 Previous micro-air vehicle research has addressed thin/cambered/reflexed airfoils on an application specific basis, relying heavily on the shape characteristics of previously designed airfoils. The motivation… (more)

Subjects/Keywords: Airfoils; Micro-air; Thin/cambered/reflexed; Vehicle; XFOIL

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APA (6th Edition):

Reid, M. (2006). Thin/cambered/reflexed airfoil development for micro-air vehicles at Reynolds numbers of 60,000 to 150,000. (Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/5781

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):

Reid, Michael. “Thin/cambered/reflexed airfoil development for micro-air vehicles at Reynolds numbers of 60,000 to 150,000.” 2006. Thesis, Rochester Institute of Technology. Accessed January 23, 2021. https://scholarworks.rit.edu/theses/5781.

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

MLA Handbook (7th Edition):

Reid, Michael. “Thin/cambered/reflexed airfoil development for micro-air vehicles at Reynolds numbers of 60,000 to 150,000.” 2006. Web. 23 Jan 2021.

Vancouver:

Reid M. Thin/cambered/reflexed airfoil development for micro-air vehicles at Reynolds numbers of 60,000 to 150,000. [Internet] [Thesis]. Rochester Institute of Technology; 2006. [cited 2021 Jan 23]. Available from: https://scholarworks.rit.edu/theses/5781.

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

Council of Science Editors:

Reid M. Thin/cambered/reflexed airfoil development for micro-air vehicles at Reynolds numbers of 60,000 to 150,000. [Thesis]. Rochester Institute of Technology; 2006. Available from: https://scholarworks.rit.edu/theses/5781

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


University of California – Irvine

18. Kiani, Mohammadali. Experimental Demonstration of the Vibrational Stability Phenomenon in Bio-inspired Flight.

Degree: Mechanical and Aerospace Engineering, 2018, University of California – Irvine

 Flapping wing micro-air-vehicles (FWMAV) are micro-air-vehicles that use biomimetic actuation (oscillatory flapping wing) for lift, propulsion, and control. The dynamic behavior of these bio-inspired systems… (more)

Subjects/Keywords: Mechanical engineering; Aerial Systems: Mechanics and Control; Bio-inspired flight; Biomimetics; Dynamics; Flapping wing micro air vehicle; Vibrational stability

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APA (6th Edition):

Kiani, M. (2018). Experimental Demonstration of the Vibrational Stability Phenomenon in Bio-inspired Flight. (Thesis). University of California – Irvine. Retrieved from http://www.escholarship.org/uc/item/8vg5j1kk

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):

Kiani, Mohammadali. “Experimental Demonstration of the Vibrational Stability Phenomenon in Bio-inspired Flight.” 2018. Thesis, University of California – Irvine. Accessed January 23, 2021. http://www.escholarship.org/uc/item/8vg5j1kk.

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

MLA Handbook (7th Edition):

Kiani, Mohammadali. “Experimental Demonstration of the Vibrational Stability Phenomenon in Bio-inspired Flight.” 2018. Web. 23 Jan 2021.

Vancouver:

Kiani M. Experimental Demonstration of the Vibrational Stability Phenomenon in Bio-inspired Flight. [Internet] [Thesis]. University of California – Irvine; 2018. [cited 2021 Jan 23]. Available from: http://www.escholarship.org/uc/item/8vg5j1kk.

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

Council of Science Editors:

Kiani M. Experimental Demonstration of the Vibrational Stability Phenomenon in Bio-inspired Flight. [Thesis]. University of California – Irvine; 2018. Available from: http://www.escholarship.org/uc/item/8vg5j1kk

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


Brigham Young University

19. Farrell, Michael David. Error-State Estimation and Control for a Multirotor UAV Landing on a Moving Vehicle.

Degree: MS, 2020, Brigham Young University

 Though multirotor unmanned aerial vehicles (UAVs) have become widely used during the past decade, challenges in autonomy have prevented their widespread use when moving vehicles… (more)

Subjects/Keywords: state estimation; optimal control; unmanned vehicles; autonomous vehicles; error state; multirotor; micro air vehicle; linear quadratic regulator; LQR; UAV; Engineering

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APA (6th Edition):

Farrell, M. D. (2020). Error-State Estimation and Control for a Multirotor UAV Landing on a Moving Vehicle. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=8879&context=etd

Chicago Manual of Style (16th Edition):

Farrell, Michael David. “Error-State Estimation and Control for a Multirotor UAV Landing on a Moving Vehicle.” 2020. Masters Thesis, Brigham Young University. Accessed January 23, 2021. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=8879&context=etd.

MLA Handbook (7th Edition):

Farrell, Michael David. “Error-State Estimation and Control for a Multirotor UAV Landing on a Moving Vehicle.” 2020. Web. 23 Jan 2021.

Vancouver:

Farrell MD. Error-State Estimation and Control for a Multirotor UAV Landing on a Moving Vehicle. [Internet] [Masters thesis]. Brigham Young University; 2020. [cited 2021 Jan 23]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=8879&context=etd.

Council of Science Editors:

Farrell MD. Error-State Estimation and Control for a Multirotor UAV Landing on a Moving Vehicle. [Masters Thesis]. Brigham Young University; 2020. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=8879&context=etd


Delft University of Technology

20. Nugteren, M. (author). Dynamic Analysis of a Resonance Based Micro Air Vehicle Structure.

Degree: 2014, Delft University of Technology

Precision and Microsystems Engineering

Mechanical, Maritime and Materials Engineering

Advisors/Committee Members: Goosen, J.F.L. (mentor), Van Keulen, A. (mentor).

Subjects/Keywords: dynamic analysis; resonance based; micro air vehicle structure

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APA (6th Edition):

Nugteren, M. (. (2014). Dynamic Analysis of a Resonance Based Micro Air Vehicle Structure. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:16cde2f5-ac05-4559-82e7-6bfaafb836f9

Chicago Manual of Style (16th Edition):

Nugteren, M (author). “Dynamic Analysis of a Resonance Based Micro Air Vehicle Structure.” 2014. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:16cde2f5-ac05-4559-82e7-6bfaafb836f9.

MLA Handbook (7th Edition):

Nugteren, M (author). “Dynamic Analysis of a Resonance Based Micro Air Vehicle Structure.” 2014. Web. 23 Jan 2021.

Vancouver:

Nugteren M(. Dynamic Analysis of a Resonance Based Micro Air Vehicle Structure. [Internet] [Masters thesis]. Delft University of Technology; 2014. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:16cde2f5-ac05-4559-82e7-6bfaafb836f9.

Council of Science Editors:

Nugteren M(. Dynamic Analysis of a Resonance Based Micro Air Vehicle Structure. [Masters Thesis]. Delft University of Technology; 2014. Available from: http://resolver.tudelft.nl/uuid:16cde2f5-ac05-4559-82e7-6bfaafb836f9


University of Maryland

21. MacFarlane, Kenneth Foster. Reduced Order Modeling of Flapping Wing Flight Dynamics.

Degree: Aerospace Engineering, 2017, University of Maryland

 Flapping wing vehicles have become a compelling alternative to classical fixed or rotary wing aircraft, especially as unmanned aircraft technology focuses on smaller, more agile… (more)

Subjects/Keywords: Aerospace engineering; flapping wing; flapping wing kinematics; flight dynamics; Insect flight; Micro air vehicle; reduced order modeling

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APA (6th Edition):

MacFarlane, K. F. (2017). Reduced Order Modeling of Flapping Wing Flight Dynamics. (Thesis). University of Maryland. Retrieved from http://hdl.handle.net/1903/19770

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):

MacFarlane, Kenneth Foster. “Reduced Order Modeling of Flapping Wing Flight Dynamics.” 2017. Thesis, University of Maryland. Accessed January 23, 2021. http://hdl.handle.net/1903/19770.

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

MLA Handbook (7th Edition):

MacFarlane, Kenneth Foster. “Reduced Order Modeling of Flapping Wing Flight Dynamics.” 2017. Web. 23 Jan 2021.

Vancouver:

MacFarlane KF. Reduced Order Modeling of Flapping Wing Flight Dynamics. [Internet] [Thesis]. University of Maryland; 2017. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/1903/19770.

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

Council of Science Editors:

MacFarlane KF. Reduced Order Modeling of Flapping Wing Flight Dynamics. [Thesis]. University of Maryland; 2017. Available from: http://hdl.handle.net/1903/19770

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


Virginia Tech

22. Stewart, Eric C. Shape and Structural Optimization of Flapping Wings.

Degree: PhD, Aerospace Engineering, 2014, Virginia Tech

 This dissertation presents shape and structural optimization studies on flapping wings for micro air vehicles. The design space of the optimization includes the wing planform… (more)

Subjects/Keywords: Flapping Wing; Micro Air Vehicle (MAV); Multi-objective Optimization; Unsteady Vortex Lattice Method (UVLM); Finite Element Analysis (FEA); Aeroelastic Optimization

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APA (6th Edition):

Stewart, E. C. (2014). Shape and Structural Optimization of Flapping Wings. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/24808

Chicago Manual of Style (16th Edition):

Stewart, Eric C. “Shape and Structural Optimization of Flapping Wings.” 2014. Doctoral Dissertation, Virginia Tech. Accessed January 23, 2021. http://hdl.handle.net/10919/24808.

MLA Handbook (7th Edition):

Stewart, Eric C. “Shape and Structural Optimization of Flapping Wings.” 2014. Web. 23 Jan 2021.

Vancouver:

Stewart EC. Shape and Structural Optimization of Flapping Wings. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/10919/24808.

Council of Science Editors:

Stewart EC. Shape and Structural Optimization of Flapping Wings. [Doctoral Dissertation]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/24808


Virginia Tech

23. Akle, Barbar Jawad. Multilayer Ionic Transducers.

Degree: MS, Mechanical Engineering, 2003, Virginia Tech

 A transducer consisting of multiple layers of ionic polymer material is developed for applications in sensing, actuation, and control. The transducer consists of two to… (more)

Subjects/Keywords: Micro Air Vehicle; Transducer; Sensor-Actuator; Ionic polymers; Multilayer

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APA (6th Edition):

Akle, B. J. (2003). Multilayer Ionic Transducers. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31733

Chicago Manual of Style (16th Edition):

Akle, Barbar Jawad. “Multilayer Ionic Transducers.” 2003. Masters Thesis, Virginia Tech. Accessed January 23, 2021. http://hdl.handle.net/10919/31733.

MLA Handbook (7th Edition):

Akle, Barbar Jawad. “Multilayer Ionic Transducers.” 2003. Web. 23 Jan 2021.

Vancouver:

Akle BJ. Multilayer Ionic Transducers. [Internet] [Masters thesis]. Virginia Tech; 2003. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/10919/31733.

Council of Science Editors:

Akle BJ. Multilayer Ionic Transducers. [Masters Thesis]. Virginia Tech; 2003. Available from: http://hdl.handle.net/10919/31733


Virginia Tech

24. Miller, Matthew Michael. Modeling, Designing, Building, and Testing a Microtubular Fuel Cell Stack Power Supply System for Micro Air Vehicle (MAVs).

Degree: MS, Mechanical Engineering, 2009, Virginia Tech

 Research and prototyping of a fuel cell stack system for micro aerial vehicles (MAVs) was conducted by Virginia Tech in collaboration with Luna Innovations, Inc,… (more)

Subjects/Keywords: Micro Air Vehicle; PEM Fuel Cell; Microtubular Fuel Cell

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APA (6th Edition):

Miller, M. M. (2009). Modeling, Designing, Building, and Testing a Microtubular Fuel Cell Stack Power Supply System for Micro Air Vehicle (MAVs). (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/76880

Chicago Manual of Style (16th Edition):

Miller, Matthew Michael. “Modeling, Designing, Building, and Testing a Microtubular Fuel Cell Stack Power Supply System for Micro Air Vehicle (MAVs).” 2009. Masters Thesis, Virginia Tech. Accessed January 23, 2021. http://hdl.handle.net/10919/76880.

MLA Handbook (7th Edition):

Miller, Matthew Michael. “Modeling, Designing, Building, and Testing a Microtubular Fuel Cell Stack Power Supply System for Micro Air Vehicle (MAVs).” 2009. Web. 23 Jan 2021.

Vancouver:

Miller MM. Modeling, Designing, Building, and Testing a Microtubular Fuel Cell Stack Power Supply System for Micro Air Vehicle (MAVs). [Internet] [Masters thesis]. Virginia Tech; 2009. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/10919/76880.

Council of Science Editors:

Miller MM. Modeling, Designing, Building, and Testing a Microtubular Fuel Cell Stack Power Supply System for Micro Air Vehicle (MAVs). [Masters Thesis]. Virginia Tech; 2009. Available from: http://hdl.handle.net/10919/76880


Wright State University

25. Duncan, Kayleigh E. Islands of Fitness Compact Genetic Algorithm for Rapid In-Flight Control Learning in a Flapping-Wing Micro Air Vehicle: A Search Space Reduction Approach.

Degree: MSCE, Computer Engineering, 2019, Wright State University

 On-going effective control of insect-scale Flapping-Wing Micro Air Vehicles could be significantly advantaged by active in-flight control adaptation. Previous work demonstrated that in simulated vehicles… (more)

Subjects/Keywords: Computer Engineering; Flapping Wing Micro Air Vehicle; Adaptive Hardware; Evolutionary Algorithm; Islands of Fitness; Compact Genetic Algorithm; Search Space Reduction

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APA (6th Edition):

Duncan, K. E. (2019). Islands of Fitness Compact Genetic Algorithm for Rapid In-Flight Control Learning in a Flapping-Wing Micro Air Vehicle: A Search Space Reduction Approach. (Masters Thesis). Wright State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=wright1578065644405701

Chicago Manual of Style (16th Edition):

Duncan, Kayleigh E. “Islands of Fitness Compact Genetic Algorithm for Rapid In-Flight Control Learning in a Flapping-Wing Micro Air Vehicle: A Search Space Reduction Approach.” 2019. Masters Thesis, Wright State University. Accessed January 23, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=wright1578065644405701.

MLA Handbook (7th Edition):

Duncan, Kayleigh E. “Islands of Fitness Compact Genetic Algorithm for Rapid In-Flight Control Learning in a Flapping-Wing Micro Air Vehicle: A Search Space Reduction Approach.” 2019. Web. 23 Jan 2021.

Vancouver:

Duncan KE. Islands of Fitness Compact Genetic Algorithm for Rapid In-Flight Control Learning in a Flapping-Wing Micro Air Vehicle: A Search Space Reduction Approach. [Internet] [Masters thesis]. Wright State University; 2019. [cited 2021 Jan 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1578065644405701.

Council of Science Editors:

Duncan KE. Islands of Fitness Compact Genetic Algorithm for Rapid In-Flight Control Learning in a Flapping-Wing Micro Air Vehicle: A Search Space Reduction Approach. [Masters Thesis]. Wright State University; 2019. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1578065644405701


Indian Institute of Science

26. Bera, Titas. Application of Randomized Algorithms in Path Planning and Control of a Micro Air Vehicle.

Degree: PhD, Faculty of Engineering, 2018, Indian Institute of Science

 This thesis focuses on the design and development of a fixed wing micro air vehicle (MAV) and on the development of randomized sampling based motion… (more)

Subjects/Keywords: Micro Air Vehicles; Fixed Wing Micro Air Vehicles; Aerodynamic Design; Computational Fluid Dynamics; Probabilistic Robust Control; Randomized Motion Planning; Narrow Passage Sampling; Rapidly Exploring Random Tree; Low Reynolds Number Aerodynamics; Fixed Wing MAVs; Micro Air Vehicle Design; Narrow Passage Sampling Algorithms; Geometric Probability; Aerospace Engineering

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APA (6th Edition):

Bera, T. (2018). Application of Randomized Algorithms in Path Planning and Control of a Micro Air Vehicle. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/3756

Chicago Manual of Style (16th Edition):

Bera, Titas. “Application of Randomized Algorithms in Path Planning and Control of a Micro Air Vehicle.” 2018. Doctoral Dissertation, Indian Institute of Science. Accessed January 23, 2021. http://etd.iisc.ac.in/handle/2005/3756.

MLA Handbook (7th Edition):

Bera, Titas. “Application of Randomized Algorithms in Path Planning and Control of a Micro Air Vehicle.” 2018. Web. 23 Jan 2021.

Vancouver:

Bera T. Application of Randomized Algorithms in Path Planning and Control of a Micro Air Vehicle. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2018. [cited 2021 Jan 23]. Available from: http://etd.iisc.ac.in/handle/2005/3756.

Council of Science Editors:

Bera T. Application of Randomized Algorithms in Path Planning and Control of a Micro Air Vehicle. [Doctoral Dissertation]. Indian Institute of Science; 2018. Available from: http://etd.iisc.ac.in/handle/2005/3756

27. Chuang, Jason C. Variable Speed Flapping Wing Micro Air Vehicle using a Continuous Variable Transmission Design.

Degree: MSEgr, Mechanical Engineering, 2014, Wright State University

 Flapping wing micro air vehicles (FWMAV) have very unique flight mechanics in two-wing orientation. Many challenges arise with two wing configuration: lift production, design construction,… (more)

Subjects/Keywords: Aerospace Engineering; MAV; micro air vehicle, CVT, continuous variable transmission; flapping wing micro air vehicle; FWMAV

…39 x CHAPTER 1 INTRODUCTION 1.1 Flapping Wing Micro Air Vehicle Flapping Wing Micro Air… …successful mission a micro air vehicle or MAV would have to sustain flight for long durations. This… …direction of flight. In retrospect micro air vehicles need the ability to autonomously control… …micro air vehicles: flapping kinematics, aerodynamic modeling, and body dynamics, according to… …3000 uses UV Curable Acrylic based plastic, the VisiJet® EX200 was used in all micro air… 

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APA (6th Edition):

Chuang, J. C. (2014). Variable Speed Flapping Wing Micro Air Vehicle using a Continuous Variable Transmission Design. (Masters Thesis). Wright State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=wright1401813452

Chicago Manual of Style (16th Edition):

Chuang, Jason C. “Variable Speed Flapping Wing Micro Air Vehicle using a Continuous Variable Transmission Design.” 2014. Masters Thesis, Wright State University. Accessed January 23, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=wright1401813452.

MLA Handbook (7th Edition):

Chuang, Jason C. “Variable Speed Flapping Wing Micro Air Vehicle using a Continuous Variable Transmission Design.” 2014. Web. 23 Jan 2021.

Vancouver:

Chuang JC. Variable Speed Flapping Wing Micro Air Vehicle using a Continuous Variable Transmission Design. [Internet] [Masters thesis]. Wright State University; 2014. [cited 2021 Jan 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1401813452.

Council of Science Editors:

Chuang JC. Variable Speed Flapping Wing Micro Air Vehicle using a Continuous Variable Transmission Design. [Masters Thesis]. Wright State University; 2014. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1401813452

28. Ameho, Yann. Du pilotage d'une famille de drones à celui d'un drone hybride via la commande adaptative : Adaptive control for a family of quadrotors and a hybrid micro air vehicle.

Degree: Docteur es, Automatique, 2013, Toulouse, ISAE

Les micro-drones sont des aéronefs sans pilotes de dimensions inférieures à un mètre et de poids inférieur à deux kilogrammes. Ils se distinguent des aéronefs… (more)

Subjects/Keywords: Micro-drone; Quadrirotor; Drone hybride; Commande adaptative; Synthèse linéaire à paramètres variants; Estimation de paramètres; Micro air vehicle; Quadrotor; Hybrid aerial vehicle; Adaptive control; Linear parameter varying control; Parameter estimation; 629.8

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APA (6th Edition):

Ameho, Y. (2013). Du pilotage d'une famille de drones à celui d'un drone hybride via la commande adaptative : Adaptive control for a family of quadrotors and a hybrid micro air vehicle. (Doctoral Dissertation). Toulouse, ISAE. Retrieved from http://www.theses.fr/2013ESAE0031

Chicago Manual of Style (16th Edition):

Ameho, Yann. “Du pilotage d'une famille de drones à celui d'un drone hybride via la commande adaptative : Adaptive control for a family of quadrotors and a hybrid micro air vehicle.” 2013. Doctoral Dissertation, Toulouse, ISAE. Accessed January 23, 2021. http://www.theses.fr/2013ESAE0031.

MLA Handbook (7th Edition):

Ameho, Yann. “Du pilotage d'une famille de drones à celui d'un drone hybride via la commande adaptative : Adaptive control for a family of quadrotors and a hybrid micro air vehicle.” 2013. Web. 23 Jan 2021.

Vancouver:

Ameho Y. Du pilotage d'une famille de drones à celui d'un drone hybride via la commande adaptative : Adaptive control for a family of quadrotors and a hybrid micro air vehicle. [Internet] [Doctoral dissertation]. Toulouse, ISAE; 2013. [cited 2021 Jan 23]. Available from: http://www.theses.fr/2013ESAE0031.

Council of Science Editors:

Ameho Y. Du pilotage d'une famille de drones à celui d'un drone hybride via la commande adaptative : Adaptive control for a family of quadrotors and a hybrid micro air vehicle. [Doctoral Dissertation]. Toulouse, ISAE; 2013. Available from: http://www.theses.fr/2013ESAE0031

29. Moses, Kenneth C. Biomimicry of the Hawk Moth, Manduca sexta (L.): Forewing and Thorax Emulation for Flapping-Wing Micro Aerial Vehicle Development.

Degree: PhD, EMC - Aerospace Engineering, 2020, Case Western Reserve University School of Graduate Studies

 For more than two decades researchers have sought to develop a micro aerial vehicle (MAV) capable of discrete remote surveillance and reconnaissance in hazardous environments… (more)

Subjects/Keywords: Aerospace Engineering; Aerospace Materials; Engineering; Mechanical Engineering; Robotics; Robots; flapping-wing micro aerial vehicle; FWMAV; flapping-wing mechanism; FWM; micro air vehicle; MAV; Manduca sexta; hawk moth; insect wing replication; thorax emulation; mechanism design; drone technology; power measurement; lift measurement

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APA (6th Edition):

Moses, K. C. (2020). Biomimicry of the Hawk Moth, Manduca sexta (L.): Forewing and Thorax Emulation for Flapping-Wing Micro Aerial Vehicle Development. (Doctoral Dissertation). Case Western Reserve University School of Graduate Studies. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=case158687503705972

Chicago Manual of Style (16th Edition):

Moses, Kenneth C. “Biomimicry of the Hawk Moth, Manduca sexta (L.): Forewing and Thorax Emulation for Flapping-Wing Micro Aerial Vehicle Development.” 2020. Doctoral Dissertation, Case Western Reserve University School of Graduate Studies. Accessed January 23, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=case158687503705972.

MLA Handbook (7th Edition):

Moses, Kenneth C. “Biomimicry of the Hawk Moth, Manduca sexta (L.): Forewing and Thorax Emulation for Flapping-Wing Micro Aerial Vehicle Development.” 2020. Web. 23 Jan 2021.

Vancouver:

Moses KC. Biomimicry of the Hawk Moth, Manduca sexta (L.): Forewing and Thorax Emulation for Flapping-Wing Micro Aerial Vehicle Development. [Internet] [Doctoral dissertation]. Case Western Reserve University School of Graduate Studies; 2020. [cited 2021 Jan 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=case158687503705972.

Council of Science Editors:

Moses KC. Biomimicry of the Hawk Moth, Manduca sexta (L.): Forewing and Thorax Emulation for Flapping-Wing Micro Aerial Vehicle Development. [Doctoral Dissertation]. Case Western Reserve University School of Graduate Studies; 2020. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=case158687503705972


Brigham Young University

30. Saunders, Jeffery Brian. Obstacle Avoidance, Visual Automatic Target Tracking, and Task Allocation for Small Unmanned Air Vehicles.

Degree: PhD, 2009, Brigham Young University

 Recent developments in autopilot technology have increased the potential use of micro air vehicles (MAVs). As the number of applications increase, the demand on MAVs… (more)

Subjects/Keywords: unmanned air vehicle; micro air vehicle; obstacle avoidance; vision-based; target tracking; task allocation; COUNTER scenario; Electrical and Computer Engineering

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APA (6th Edition):

Saunders, J. B. (2009). Obstacle Avoidance, Visual Automatic Target Tracking, and Task Allocation for Small Unmanned Air Vehicles. (Doctoral Dissertation). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=2856&context=etd

Chicago Manual of Style (16th Edition):

Saunders, Jeffery Brian. “Obstacle Avoidance, Visual Automatic Target Tracking, and Task Allocation for Small Unmanned Air Vehicles.” 2009. Doctoral Dissertation, Brigham Young University. Accessed January 23, 2021. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=2856&context=etd.

MLA Handbook (7th Edition):

Saunders, Jeffery Brian. “Obstacle Avoidance, Visual Automatic Target Tracking, and Task Allocation for Small Unmanned Air Vehicles.” 2009. Web. 23 Jan 2021.

Vancouver:

Saunders JB. Obstacle Avoidance, Visual Automatic Target Tracking, and Task Allocation for Small Unmanned Air Vehicles. [Internet] [Doctoral dissertation]. Brigham Young University; 2009. [cited 2021 Jan 23]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=2856&context=etd.

Council of Science Editors:

Saunders JB. Obstacle Avoidance, Visual Automatic Target Tracking, and Task Allocation for Small Unmanned Air Vehicles. [Doctoral Dissertation]. Brigham Young University; 2009. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=2856&context=etd

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