subject:(MAV)

Delft University of Technology

1. Van Hecke, K.G. Persistent self-supervised learning principle: Study and demonstration on flying robots:.

Degree: 2015, Delft University of Technology

URL: http://resolver.tudelft.nl/uuid:b722da02-089f-42a8-a3ea-fb3f5900bcdd

► We introduce, study and demonstrate Persistent Self-Supervised Learning (PSSL), a machine learning method for usage onboard robotic platforms. The PSSL model leverages a standard supervised… (more)

Subjects/Keywords: persistent self-supervised learning; MAV

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APA (6^th Edition):

Van Hecke, K. G. (2015). Persistent self-supervised learning principle: Study and demonstration on flying robots:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:b722da02-089f-42a8-a3ea-fb3f5900bcdd

Chicago Manual of Style (16^th Edition):

Van Hecke, K G. “Persistent self-supervised learning principle: Study and demonstration on flying robots:.” 2015. Masters Thesis, Delft University of Technology. Accessed December 11, 2019. http://resolver.tudelft.nl/uuid:b722da02-089f-42a8-a3ea-fb3f5900bcdd.

MLA Handbook (7^th Edition):

Van Hecke, K G. “Persistent self-supervised learning principle: Study and demonstration on flying robots:.” 2015. Web. 11 Dec 2019.

Vancouver:

Van Hecke KG. Persistent self-supervised learning principle: Study and demonstration on flying robots:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Dec 11]. Available from: http://resolver.tudelft.nl/uuid:b722da02-089f-42a8-a3ea-fb3f5900bcdd.

Council of Science Editors:

Van Hecke KG. Persistent self-supervised learning principle: Study and demonstration on flying robots:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:b722da02-089f-42a8-a3ea-fb3f5900bcdd

Rice University

2. Buscher, Austin J. Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces.

Degree: MS, Mechanical Engineering, 2014, Rice University

URL: http://hdl.handle.net/1911/103780

► To address the computational challenges associated with contact between moving solid surfaces, such as those in cardiovascular fluid–structure interaction (FSI), parachute FSI, and flapping-wing aerodynamics,… (more)

Subjects/Keywords: space – time; toplogy-change; MAV; heart valve

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

APA (6^th Edition):

Buscher, A. J. (2014). Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/103780

Chicago Manual of Style (16^th Edition):

Buscher, Austin J. “Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces.” 2014. Masters Thesis, Rice University. Accessed December 11, 2019. http://hdl.handle.net/1911/103780.

MLA Handbook (7^th Edition):

Buscher, Austin J. “Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces.” 2014. Web. 11 Dec 2019.

Vancouver:

Buscher AJ. Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces. [Internet] [Masters thesis]. Rice University; 2014. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/1911/103780.

Council of Science Editors:

Buscher AJ. Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces. [Masters Thesis]. Rice University; 2014. Available from: http://hdl.handle.net/1911/103780

Delft University of Technology

3. Selvan, A. Simulation of optic flow based flight control for a flapping wing micro aerial vehicle:.

Degree: 2014, Delft University of Technology

URL: http://resolver.tudelft.nl/uuid:4c93976d-8ae2-4913-bf5d-c56408f4ccc3

► Bio-inspired flying micro drones, formally known as Flapping Wing Micro Aerial Vehicles (FWMAV) are a booming class of robots in today's world. Navigation and flight… (more)

Subjects/Keywords: FWMAV; MAV; Optic flow; Flight control

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APA (6^th Edition):

Selvan, A. (2014). Simulation of optic flow based flight control for a flapping wing micro aerial vehicle:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:4c93976d-8ae2-4913-bf5d-c56408f4ccc3

Chicago Manual of Style (16^th Edition):

Selvan, A. “Simulation of optic flow based flight control for a flapping wing micro aerial vehicle:.” 2014. Masters Thesis, Delft University of Technology. Accessed December 11, 2019. http://resolver.tudelft.nl/uuid:4c93976d-8ae2-4913-bf5d-c56408f4ccc3.

MLA Handbook (7^th Edition):

Selvan, A. “Simulation of optic flow based flight control for a flapping wing micro aerial vehicle:.” 2014. Web. 11 Dec 2019.

Vancouver:

Selvan A. Simulation of optic flow based flight control for a flapping wing micro aerial vehicle:. [Internet] [Masters thesis]. Delft University of Technology; 2014. [cited 2019 Dec 11]. Available from: http://resolver.tudelft.nl/uuid:4c93976d-8ae2-4913-bf5d-c56408f4ccc3.

Council of Science Editors:

Selvan A. Simulation of optic flow based flight control for a flapping wing micro aerial vehicle:. [Masters Thesis]. Delft University of Technology; 2014. Available from: http://resolver.tudelft.nl/uuid:4c93976d-8ae2-4913-bf5d-c56408f4ccc3

Delft University of Technology

4. Jain, R.P.K. Transportation of Cable Suspended Load using Unmanned Aerial Vehicles: A Real-time Model Predictive Control approach:.

Degree: 2015, Delft University of Technology

URL: http://resolver.tudelft.nl/uuid:4c6b4a94-4f15-4e67-8c30-eb8156aab406

► Unmanned Aerial Vehicles (UAV) have received an increasing amount of attention recently with many applications being actively investigated across the globe, and several related open… (more)

▼ Unmanned Aerial Vehicles (UAV) have received an increasing amount of attention recently with many applications being actively investigated across the globe, and several related open research questions being actively pursued. Possible applications include search and rescue, disaster relief, environmental monitoring and surveillance, transportation, and construction. Transportation of cable suspended payloads using Unmanned Aerial Vehicles is one such application which is the topic of this research. Autonomous transportation of objects using UAV can contribute to the safe and reliable supply of food and medicine in remote or disaster-affected areas and even in commercial delivery of goods. The state-of-the-art approaches towards the slung load transportation either develop non-linear feedback control laws to stabilize the system to a predefined trajectory or employ open loop off-line trajectory planning schemes to generate optimal control inputs to the system. Most of these techniques often rely on availability of an accurate model of the system backed up with simulation results. Very few results exist which target experimental validation of the proposed method. Based on the findings of the previously conducted literature survey, it appears that the application of closed loop on-line trajectory generation and control schemes to transport a slung payload in swing free manner remains unanswered. The work in this thesis sets off to answer the research questions in this direction and address the issues that come along with experimental validation. Model Predictive Control (MPC) is a promising framework, which provides the means to tackle both the trajectory generation problem and the feedback control problem in an unified manner. As a result, it forms the most important component of this thesis. Specific research problem that is addressed in this thesis is to transport a cable suspended load using quadrotor from one point to another, while minimizing the swing through the use of Linear Time Invariant MPC techniques. A non-linear dynamic model for the quadrotor-slung load system is obtained and the structure within the system dynamics is exploited to decide the control strategy. Two different MPC formulations viz. MPC with integral action and MPC with delta-u formulation are simulated and compared to Linear Quadratic control with integral action which acts as a benchmark controller. Backed with simulation results, it is shown through experimental validation that it is possible to control the swing of cable suspended load using linear control techniques. MPC being an computationally expensive task, state-of-the-art fast optimization solvers such as FORCES PRO is used to achieve on-line implementation of MPC for the quadrotor-slung load system. To this end, a new software framework for implementation of MPC is developed which establishes a wireless link with the quadrotor resulting in a real-time networked control loop. Advisors/Committee Members: Keviczky, T..

Subjects/Keywords: quadrotor; model predictive control; paparazzi; MAV; robotics

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APA (6^th Edition):

Jain, R. P. K. (2015). Transportation of Cable Suspended Load using Unmanned Aerial Vehicles: A Real-time Model Predictive Control approach:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:4c6b4a94-4f15-4e67-8c30-eb8156aab406

Chicago Manual of Style (16^th Edition):

Jain, R P K. “Transportation of Cable Suspended Load using Unmanned Aerial Vehicles: A Real-time Model Predictive Control approach:.” 2015. Masters Thesis, Delft University of Technology. Accessed December 11, 2019. http://resolver.tudelft.nl/uuid:4c6b4a94-4f15-4e67-8c30-eb8156aab406.

MLA Handbook (7^th Edition):

Jain, R P K. “Transportation of Cable Suspended Load using Unmanned Aerial Vehicles: A Real-time Model Predictive Control approach:.” 2015. Web. 11 Dec 2019.

Vancouver:

Jain RPK. Transportation of Cable Suspended Load using Unmanned Aerial Vehicles: A Real-time Model Predictive Control approach:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Dec 11]. Available from: http://resolver.tudelft.nl/uuid:4c6b4a94-4f15-4e67-8c30-eb8156aab406.

Council of Science Editors:

Jain RPK. Transportation of Cable Suspended Load using Unmanned Aerial Vehicles: A Real-time Model Predictive Control approach:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:4c6b4a94-4f15-4e67-8c30-eb8156aab406

George Mason University

5. Garrity, Michael J. Computational Membrane Model Using Finite Element Method for Flexible-Wing Based Micro Air Vehicles .

Degree: 2011, George Mason University

URL: http://hdl.handle.net/1920/6605

► Current designs for Micro Air Vehicles (MAVs) consist of a flexible wing with rigid battens for support. This paper analyzes the development and evaluation of… (more)

Subjects/Keywords: Membrane; MAV; Flexible; Hyperelasticity; Model; C++

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APA (6^th Edition):

Garrity, M. J. (2011). Computational Membrane Model Using Finite Element Method for Flexible-Wing Based Micro Air Vehicles . (Thesis). George Mason University. Retrieved from http://hdl.handle.net/1920/6605

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

Chicago Manual of Style (16^th Edition):

Garrity, Michael J. “Computational Membrane Model Using Finite Element Method for Flexible-Wing Based Micro Air Vehicles .” 2011. Thesis, George Mason University. Accessed December 11, 2019. http://hdl.handle.net/1920/6605.

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

MLA Handbook (7^th Edition):

Garrity, Michael J. “Computational Membrane Model Using Finite Element Method for Flexible-Wing Based Micro Air Vehicles .” 2011. Web. 11 Dec 2019.

Vancouver:

Garrity MJ. Computational Membrane Model Using Finite Element Method for Flexible-Wing Based Micro Air Vehicles . [Internet] [Thesis]. George Mason University; 2011. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/1920/6605.

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

Council of Science Editors:

Garrity MJ. Computational Membrane Model Using Finite Element Method for Flexible-Wing Based Micro Air Vehicles . [Thesis]. George Mason University; 2011. Available from: http://hdl.handle.net/1920/6605

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

Rice University

6. Buscher, Austin J. Space–Time Interface–Tracking Computations with Contact Between Solid Surfaces.

Degree: MS, Mechanical Engineering, 2014, Rice University

URL: http://hdl.handle.net/1911/87723

► To address the computational challenges associated with contact between moving solid surfaces, such as those in cardiovascular fluid–structure interaction (FSI), parachute FSI, and flapping-wing aerodynamics,… (more)

Subjects/Keywords: space – time; toplogy-change; MAV; heart valve

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

APA (6^th Edition):

Buscher, A. J. (2014). Space–Time Interface–Tracking Computations with Contact Between Solid Surfaces. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/87723

Chicago Manual of Style (16^th Edition):

Buscher, Austin J. “Space–Time Interface–Tracking Computations with Contact Between Solid Surfaces.” 2014. Masters Thesis, Rice University. Accessed December 11, 2019. http://hdl.handle.net/1911/87723.

MLA Handbook (7^th Edition):

Buscher, Austin J. “Space–Time Interface–Tracking Computations with Contact Between Solid Surfaces.” 2014. Web. 11 Dec 2019.

Vancouver:

Buscher AJ. Space–Time Interface–Tracking Computations with Contact Between Solid Surfaces. [Internet] [Masters thesis]. Rice University; 2014. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/1911/87723.

Council of Science Editors:

Buscher AJ. Space–Time Interface–Tracking Computations with Contact Between Solid Surfaces. [Masters Thesis]. Rice University; 2014. Available from: http://hdl.handle.net/1911/87723

7. Bolsman, C.T. Flapping wing actuation using resonant compliant mechanisms: An insect-inspired design.

Degree: 2010, Ipskamp

URL: http://resolver.tudelft.nl/uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a ; urn:NBN:nl:ui:24-uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a ; urn:NBN:nl:ui:24-uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a ; http://resolver.tudelft.nl/uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a

► The realization of a wing actuation mechanism for a flapping wing micro air vehicle requires a move away from traditional designs based on gears and… (more)

Subjects/Keywords: flapping wing MAV

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APA (6^th Edition):

Bolsman, C. T. (2010). Flapping wing actuation using resonant compliant mechanisms: An insect-inspired design. (Doctoral Dissertation). Ipskamp. Retrieved from http://resolver.tudelft.nl/uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a ; urn:NBN:nl:ui:24-uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a ; urn:NBN:nl:ui:24-uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a ; http://resolver.tudelft.nl/uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a

Chicago Manual of Style (16^th Edition):

Bolsman, C T. “Flapping wing actuation using resonant compliant mechanisms: An insect-inspired design.” 2010. Doctoral Dissertation, Ipskamp. Accessed December 11, 2019. http://resolver.tudelft.nl/uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a ; urn:NBN:nl:ui:24-uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a ; urn:NBN:nl:ui:24-uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a ; http://resolver.tudelft.nl/uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a.

MLA Handbook (7^th Edition):

Bolsman, C T. “Flapping wing actuation using resonant compliant mechanisms: An insect-inspired design.” 2010. Web. 11 Dec 2019.

Vancouver:

Bolsman CT. Flapping wing actuation using resonant compliant mechanisms: An insect-inspired design. [Internet] [Doctoral dissertation]. Ipskamp; 2010. [cited 2019 Dec 11]. Available from: http://resolver.tudelft.nl/uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a ; urn:NBN:nl:ui:24-uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a ; urn:NBN:nl:ui:24-uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a ; http://resolver.tudelft.nl/uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a.

Council of Science Editors:

Bolsman CT. Flapping wing actuation using resonant compliant mechanisms: An insect-inspired design. [Doctoral Dissertation]. Ipskamp; 2010. Available from: http://resolver.tudelft.nl/uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a ; urn:NBN:nl:ui:24-uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a ; urn:NBN:nl:ui:24-uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a ; http://resolver.tudelft.nl/uuid:9c277bea-9b50-4ba4-82c5-09083ffe053a

Rice University

8. Buscher, Austin J. Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces.

Degree: MS, Engineering, 2014, Rice University

URL: http://hdl.handle.net/1911/103866

► To address the computational challenges associated with contact between moving solid surfaces, such as those in cardiovascular fluid–structure interaction (FSI), parachute FSI, and flapping-wing aerodynamics,… (more)

Subjects/Keywords: space – time; toplogy-change; MAV; heart valve

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

APA (6^th Edition):

Buscher, A. J. (2014). Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces. (Masters Thesis). Rice University. Retrieved from http://hdl.handle.net/1911/103866

Chicago Manual of Style (16^th Edition):

Buscher, Austin J. “Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces.” 2014. Masters Thesis, Rice University. Accessed December 11, 2019. http://hdl.handle.net/1911/103866.

MLA Handbook (7^th Edition):

Buscher, Austin J. “Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces.” 2014. Web. 11 Dec 2019.

Vancouver:

Buscher AJ. Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces. [Internet] [Masters thesis]. Rice University; 2014. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/1911/103866.

Council of Science Editors:

Buscher AJ. Space–Time Interface-Tracking Computations with Contact Between Solid Surfaces. [Masters Thesis]. Rice University; 2014. Available from: http://hdl.handle.net/1911/103866

Brno University of Technology

9. Krejčí, Jan. Přehled miniaturních bezpilotních prostředků .

Degree: 2012, Brno University of Technology

URL: http://hdl.handle.net/11012/5157

► Bakalářská práce se zabývá přehledem miniaturních bezpilotních letounů. Je zde uveden jejich stručný historický vývoj, rozdělení bezpilotních prostředků a vymezení kategorie MAV, přehled vybraných zástupců… (more)

Subjects/Keywords: Miniaturní bezpilotní prostředek; MAV; přehled; historie; použití; umělá inteligence; Miniature aerial vehicle; MAV; overview; history; application; artificial intelligence

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APA (6^th Edition):

Krejčí, J. (2012). Přehled miniaturních bezpilotních prostředků . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/5157

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

Chicago Manual of Style (16^th Edition):

Krejčí, Jan. “Přehled miniaturních bezpilotních prostředků .” 2012. Thesis, Brno University of Technology. Accessed December 11, 2019. http://hdl.handle.net/11012/5157.

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

MLA Handbook (7^th Edition):

Krejčí, Jan. “Přehled miniaturních bezpilotních prostředků .” 2012. Web. 11 Dec 2019.

Vancouver:

Krejčí J. Přehled miniaturních bezpilotních prostředků . [Internet] [Thesis]. Brno University of Technology; 2012. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/11012/5157.

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

Council of Science Editors:

Krejčí J. Přehled miniaturních bezpilotních prostředků . [Thesis]. Brno University of Technology; 2012. Available from: http://hdl.handle.net/11012/5157

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

KTH

10. Greenberg, Jacob. Visual Odometry for Autonomous MAV with On-Board Processing.

Degree: Computer Science and Communication (CSC), 2015, KTH

URL: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-177290

►

A new visual registration algorithm (Adaptive Iterative Closest Keypoint, AICK) is tested and evaluated as a positioning tool on a Micro Aerial Vehicle (MAV).… (more)

▼

A new visual registration algorithm (Adaptive Iterative Closest Keypoint, AICK) is tested and evaluated as a positioning tool on a Micro Aerial Vehicle (MAV). Captured frames from a Kinect like RGB-D camera are analyzed and an estimated position of the MAV is extracted. The hope is to find a positioning solution for GPS-denied environments. This thesis is focused on an indoor office environment. The MAV is flown manually, capturing in-flight RGB-D images which are registered with the AICK algorithm. The result is analyzed to come to a conclusion if AICK is viable or not for autonomous flight based on on-board positioning estimates. The result shows potential for a working autonomous MAV in GPS-denied environments, however there are some surroundings that have proven difficult. The lack of visual features on e.g., a white wall causes problems and uncertainties in the positioning, which is even more troublesome when the distance to the surroundings exceed the RGB-D cameras depth range. With further work on these weaknesses we believe that a robust autonomous MAV using AICK for positioning is plausible.

En ny visuell registreringsalgoritm (Adaptive Iterative Closest Keypoint, AICK) testas och utvärderas som ett positioneringsverktyg på en Micro Aerial Vehicle (MAV). Tagna bilder från en Kinect liknande RGB-D kamera analyseras och en approximerad position av MAVen beräknas. Förhoppningen är att hitta en positioneringslösning för miljöer utan GPS förbindelse, där detta arbete fokuserar på kontorsmiljöer inomhus. MAVen flygs manuellt samtidigt som RGB-D bilder tas, dessa registreras sedan med hjälp av AICK. Resultatet analyseras för att kunna dra en slutsats om AICK är en rimlig metod eller inte för att åstadkomma autonom flygning med hjälp av den uppskattade positionen. Resultatet visar potentialen för en fungerande autonom MAV i miljöer utan GPS förbindelse, men det finns testade miljöer där AICK i dagsläget fungerar undermåligt. Bristen på visuella särdrag på t.ex. en vit vägg inför problem och osäkerheter i positioneringen, ännu mer besvärande är det när avståndet till omgivningen överskrider RGB-D kamerornas räckvidd. Med fortsatt arbete med dessa svagheter är en robust autonom MAV som använder AICK för positioneringen rimlig.

Subjects/Keywords: MAV; Visual Odometry; AICK; Computer Sciences; Datavetenskap (datalogi)

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APA (6^th Edition):

Greenberg, J. (2015). Visual Odometry for Autonomous MAV with On-Board Processing. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-177290

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

Chicago Manual of Style (16^th Edition):

Greenberg, Jacob. “Visual Odometry for Autonomous MAV with On-Board Processing.” 2015. Thesis, KTH. Accessed December 11, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-177290.

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

MLA Handbook (7^th Edition):

Greenberg, Jacob. “Visual Odometry for Autonomous MAV with On-Board Processing.” 2015. Web. 11 Dec 2019.

Vancouver:

Greenberg J. Visual Odometry for Autonomous MAV with On-Board Processing. [Internet] [Thesis]. KTH; 2015. [cited 2019 Dec 11]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-177290.

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

Council of Science Editors:

Greenberg J. Visual Odometry for Autonomous MAV with On-Board Processing. [Thesis]. KTH; 2015. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-177290

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

11. Salichon, Max. Learning based methods applied to the MAV control problem.

Degree: PhD, Mechanical Engineering, 2009, Oregon State University

URL: http://hdl.handle.net/1957/13669

► This thesis addresses Micro Aerial Vehicle (MAV) control by leveraging learning based techniques to improve robustness of the control system. Applying classical control methods to… (more)

Subjects/Keywords: MAV; Micro air vehicles

…2.3.2 Flexible-wing MAV . . . . . . . 2.3.3 UAV… …3 MAV Model, System dynamics, and Basic Control 46 3.1 MAV Platform: GENMAV… …System Dynamics: AVL / JSBSim . . . . . . . . . . . . . . . . . . 49 3.4 MAV Control… …prediction code. AVL calculates forces and moments applied to the MAV as well as the lift and drag… …which in return provides the MAV states. . . . . . . . . . . . . . . . . . . . . 54 Neuro…

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

APA (6^th Edition):

Salichon, M. (2009). Learning based methods applied to the MAV control problem. (Doctoral Dissertation). Oregon State University. Retrieved from http://hdl.handle.net/1957/13669

Chicago Manual of Style (16^th Edition):

Salichon, Max. “Learning based methods applied to the MAV control problem.” 2009. Doctoral Dissertation, Oregon State University. Accessed December 11, 2019. http://hdl.handle.net/1957/13669.

MLA Handbook (7^th Edition):

Salichon, Max. “Learning based methods applied to the MAV control problem.” 2009. Web. 11 Dec 2019.

Vancouver:

Salichon M. Learning based methods applied to the MAV control problem. [Internet] [Doctoral dissertation]. Oregon State University; 2009. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/1957/13669.

Council of Science Editors:

Salichon M. Learning based methods applied to the MAV control problem. [Doctoral Dissertation]. Oregon State University; 2009. Available from: http://hdl.handle.net/1957/13669

EPFL

12. Bouabdallah, Samir. Design and control of quadrotors with application to autonomous flying.

Degree: 2007, EPFL

URL: http://infoscience.epfl.ch/record/95939

► This thesis is about modelling, design and control of Miniature Flying Robots (MFR) with a focus on Vertical Take-Off and Landing (VTOL) systems and specifically,… (more)

Subjects/Keywords: Quadrotor; Dynamic Modelling; Backstepping; MAV

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APA (6^th Edition):

Bouabdallah, S. (2007). Design and control of quadrotors with application to autonomous flying. (Thesis). EPFL. Retrieved from http://infoscience.epfl.ch/record/95939

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

Chicago Manual of Style (16^th Edition):

Bouabdallah, Samir. “Design and control of quadrotors with application to autonomous flying.” 2007. Thesis, EPFL. Accessed December 11, 2019. http://infoscience.epfl.ch/record/95939.

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

MLA Handbook (7^th Edition):

Bouabdallah, Samir. “Design and control of quadrotors with application to autonomous flying.” 2007. Web. 11 Dec 2019.

Vancouver:

Bouabdallah S. Design and control of quadrotors with application to autonomous flying. [Internet] [Thesis]. EPFL; 2007. [cited 2019 Dec 11]. Available from: http://infoscience.epfl.ch/record/95939.

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

Council of Science Editors:

Bouabdallah S. Design and control of quadrotors with application to autonomous flying. [Thesis]. EPFL; 2007. Available from: http://infoscience.epfl.ch/record/95939

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

Oregon State University

13. Wilcox, Joshua Robert. Non-Isotropic Fiber Reinforced Elastic Membranes for Micro Aerial Vehicle Wings.

Degree: MS, Mechanical Engineering, 2015, Oregon State University

URL: http://hdl.handle.net/1957/56256

► Micro air vehicles (MAV's) and small unmanned aerial vehicles (SUAV) are remotely piloted or autonomous aircraft with a take-off mass range between 50 g and… (more)

Subjects/Keywords: MAV; Micro air vehicles – Wings – Design and construction

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APA (6^th Edition):

Wilcox, J. R. (2015). Non-Isotropic Fiber Reinforced Elastic Membranes for Micro Aerial Vehicle Wings. (Masters Thesis). Oregon State University. Retrieved from http://hdl.handle.net/1957/56256

Chicago Manual of Style (16^th Edition):

Wilcox, Joshua Robert. “Non-Isotropic Fiber Reinforced Elastic Membranes for Micro Aerial Vehicle Wings.” 2015. Masters Thesis, Oregon State University. Accessed December 11, 2019. http://hdl.handle.net/1957/56256.

MLA Handbook (7^th Edition):

Wilcox, Joshua Robert. “Non-Isotropic Fiber Reinforced Elastic Membranes for Micro Aerial Vehicle Wings.” 2015. Web. 11 Dec 2019.

Vancouver:

Wilcox JR. Non-Isotropic Fiber Reinforced Elastic Membranes for Micro Aerial Vehicle Wings. [Internet] [Masters thesis]. Oregon State University; 2015. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/1957/56256.

Council of Science Editors:

Wilcox JR. Non-Isotropic Fiber Reinforced Elastic Membranes for Micro Aerial Vehicle Wings. [Masters Thesis]. Oregon State University; 2015. Available from: http://hdl.handle.net/1957/56256

Case Western Reserve University

14. Bachmann, Richard Joseph. A Hybrid Vehicle for Aerial and Terrestrial Locomotion.

Degree: PhD, EMC - Mechanical Engineering, 2009, Case Western Reserve University

URL: http://rave.ohiolink.edu/etdc/view?acc_num=case1232735399

► A durable hybrid vehicle has been developed capable of both aerial and terrestrial locomotion. The motivation for the work was a wide range of sensor… (more)

▼ A durable hybrid vehicle has been developed capable of both aerial and terrestrial locomotion. The motivation for the work was a wide range of sensor deployment scenarios that would benefit from a vehicle capable of 1) flying long distances to a target area and 2) walking around the target to perform near-field inspection. A technology survey was performed to identify the candidate terrestrial and aerial locomotion technologies for integration. The Mini-Whegs robot, developed at Case Western Reserve University, was selected as the terrestrial running gear, and the flexible-wing micro air vehicle (MAV), developed at University of Florida, was selected as the aerial platform. A rigorous trade-off analysis led to a remote control prototype that had a fully functional airframe augmented with two R/C servos, modified for continuous rotation, driving independent music wire wheel-legs at the front of the vehicle. This vehicle achieved most of the original performance requirements. It could fly, land, crawl, and regain flight by crawling off the edge of a rooftop. A critical performance evaluation illuminated improvements to the design and fabrication necessary to create a viable hybrid vehicle for field deployment. The vehicle design and fabrication processes were overhauled to improve the durability and reproducibility of the final design. A custom-built terrestrial locomotion subsystem, with compliance in the drive train, was crucial to improved durability. CNC fabrication of the fuselage mold and a one-piece tail design were central to repeatability. A commercially available autopilot was implemented for autonomous operation. Vehicle mass increased from 118 to 365 grams. The wingspan was subsequently increased to 16", but wing loading increased from 37 to 64 N/m². A corresponding decrease in controllability was observed. Winglets were found to increase lift, but decrease stability by mitigating wing flexibility. The final vehicle was able to fly, land, and crawl repeatedly. Over 8 flights (and landings) have been performed by the vehicle, and the vehicle has yet to show any signs of damage. The vehicle cruises at 14 m/s and crawls at 0.33 m/s (0.8 body lengths per second). For comparison, a typical Mini-Whegs runs at 5 body lengths per second. Advisors/Committee Members: Quinn, Roger (Advisor).

Subjects/Keywords: Mechanical Engineering; hybrid; locomotion; MAV; Whegs; terrestrial; aerial; integration

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APA (6^th Edition):

Bachmann, R. J. (2009). A Hybrid Vehicle for Aerial and Terrestrial Locomotion. (Doctoral Dissertation). Case Western Reserve University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=case1232735399

Chicago Manual of Style (16^th Edition):

Bachmann, Richard Joseph. “A Hybrid Vehicle for Aerial and Terrestrial Locomotion.” 2009. Doctoral Dissertation, Case Western Reserve University. Accessed December 11, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=case1232735399.

MLA Handbook (7^th Edition):

Bachmann, Richard Joseph. “A Hybrid Vehicle for Aerial and Terrestrial Locomotion.” 2009. Web. 11 Dec 2019.

Vancouver:

Bachmann RJ. A Hybrid Vehicle for Aerial and Terrestrial Locomotion. [Internet] [Doctoral dissertation]. Case Western Reserve University; 2009. [cited 2019 Dec 11]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=case1232735399.

Council of Science Editors:

Bachmann RJ. A Hybrid Vehicle for Aerial and Terrestrial Locomotion. [Doctoral Dissertation]. Case Western Reserve University; 2009. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=case1232735399

Penn State University

15. Corbets, Jeffrey. Real-Time Trajectory Generation for Target Localization Using Micro Air Vehicles.

Degree: MS, Aerospace Engineering, 2008, Penn State University

URL: https://etda.libraries.psu.edu/catalog/8672

► This thesis presents an approach to near-optimal target localization for small and micro unmanned aerial vehicles using a family of pre-computed parameterized trajectories. These trajectories… (more)

Subjects/Keywords: uav; mav; localization; planning; path; trajectory; real time; micro; target; tracking

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APA (6^th Edition):

Corbets, J. (2008). Real-Time Trajectory Generation for Target Localization Using Micro Air Vehicles. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/8672

Chicago Manual of Style (16^th Edition):

Corbets, Jeffrey. “Real-Time Trajectory Generation for Target Localization Using Micro Air Vehicles.” 2008. Masters Thesis, Penn State University. Accessed December 11, 2019. https://etda.libraries.psu.edu/catalog/8672.

MLA Handbook (7^th Edition):

Corbets, Jeffrey. “Real-Time Trajectory Generation for Target Localization Using Micro Air Vehicles.” 2008. Web. 11 Dec 2019.

Vancouver:

Corbets J. Real-Time Trajectory Generation for Target Localization Using Micro Air Vehicles. [Internet] [Masters thesis]. Penn State University; 2008. [cited 2019 Dec 11]. Available from: https://etda.libraries.psu.edu/catalog/8672.

Council of Science Editors:

Corbets J. Real-Time Trajectory Generation for Target Localization Using Micro Air Vehicles. [Masters Thesis]. Penn State University; 2008. Available from: https://etda.libraries.psu.edu/catalog/8672

Harvard University

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

Degree: PhD, Engineering Sciences, 2012, Harvard University

URL: http://nrs.harvard.edu/urn-3:HUL.InstRepos:9920663

►

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 (6^th 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 (16^th Edition):

Finio, Benjamin. “Roll, Pitch and Yaw Torque Control for a Robotic Bee.” 2012. Doctoral Dissertation, Harvard University. Accessed December 11, 2019. http://nrs.harvard.edu/urn-3:HUL.InstRepos:9920663.

MLA Handbook (7^th Edition):

Finio, Benjamin. “Roll, Pitch and Yaw Torque Control for a Robotic Bee.” 2012. Web. 11 Dec 2019.

Vancouver:

Finio B. Roll, Pitch and Yaw Torque Control for a Robotic Bee. [Internet] [Doctoral dissertation]. Harvard University; 2012. [cited 2019 Dec 11]. 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

17. Sreetharan, Pratheev Sabaratnam. Mechanical Intelligence in Millimeter-Scale Machines.

Degree: PhD, Applied Physics, 2012, Harvard University

URL: http://nrs.harvard.edu/urn-3:HUL.InstRepos:10085979

►

Advances in millimeter-scale fabrication processes have enabled rapid progress towards the development of flapping wing micro air vehicles with wing spans of several centimeters and… (more)

Subjects/Keywords: MAV; MEMS; microrobotics; robotics

11 more images…

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APA (6^th Edition):

Sreetharan, P. S. (2012). Mechanical Intelligence in Millimeter-Scale Machines. (Doctoral Dissertation). Harvard University. Retrieved from http://nrs.harvard.edu/urn-3:HUL.InstRepos:10085979

Chicago Manual of Style (16^th Edition):

Sreetharan, Pratheev Sabaratnam. “Mechanical Intelligence in Millimeter-Scale Machines.” 2012. Doctoral Dissertation, Harvard University. Accessed December 11, 2019. http://nrs.harvard.edu/urn-3:HUL.InstRepos:10085979.

MLA Handbook (7^th Edition):

Sreetharan, Pratheev Sabaratnam. “Mechanical Intelligence in Millimeter-Scale Machines.” 2012. Web. 11 Dec 2019.

Vancouver:

Sreetharan PS. Mechanical Intelligence in Millimeter-Scale Machines. [Internet] [Doctoral dissertation]. Harvard University; 2012. [cited 2019 Dec 11]. Available from: http://nrs.harvard.edu/urn-3:HUL.InstRepos:10085979.

Council of Science Editors:

Sreetharan PS. Mechanical Intelligence in Millimeter-Scale Machines. [Doctoral Dissertation]. Harvard University; 2012. Available from: http://nrs.harvard.edu/urn-3:HUL.InstRepos:10085979

18. Sharma, Aman. System Identification of a Micro Aerial Vehicle.

Degree: Space Technology, 2019, Luleå University of Technology

URL: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-73070

► The purpose of this thesis was to implement an Model Predictive Control based system identification method on a micro-aerial vehicle (DJI Matrice 100) as… (more)

Subjects/Keywords: Drones; MAV; Control Engineering; System Identification; Control Engineering; Reglerteknik

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APA (6^th Edition):

Sharma, A. (2019). System Identification of a Micro Aerial Vehicle. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-73070

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

Chicago Manual of Style (16^th Edition):

Sharma, Aman. “System Identification of a Micro Aerial Vehicle.” 2019. Thesis, Luleå University of Technology. Accessed December 11, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-73070.

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

MLA Handbook (7^th Edition):

Sharma, Aman. “System Identification of a Micro Aerial Vehicle.” 2019. Web. 11 Dec 2019.

Vancouver:

Sharma A. System Identification of a Micro Aerial Vehicle. [Internet] [Thesis]. Luleå University of Technology; 2019. [cited 2019 Dec 11]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-73070.

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

Council of Science Editors:

Sharma A. System Identification of a Micro Aerial Vehicle. [Thesis]. Luleå University of Technology; 2019. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-73070

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

Rochester Institute of Technology

19. Hollenbach, Andrew. Low-Cost Multiple-MAV SLAM Using Open Source Software.

Degree: MS, Computer Science (GCCIS), 2018, Rochester Institute of Technology

URL: https://scholarworks.rit.edu/theses/9861

► We demonstrate a multiple micro aerial vehicle (MAV) system capable of supporting autonomous exploration and navigation in unknown environments using only a sensor commonly… (more)

Subjects/Keywords: Cooperative; MAV; Monocular; Real-time systems; SLAM; UAV

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APA (6^th Edition):

Hollenbach, A. (2018). Low-Cost Multiple-MAV SLAM Using Open Source Software. (Masters Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/9861

Chicago Manual of Style (16^th Edition):

Hollenbach, Andrew. “Low-Cost Multiple-MAV SLAM Using Open Source Software.” 2018. Masters Thesis, Rochester Institute of Technology. Accessed December 11, 2019. https://scholarworks.rit.edu/theses/9861.

MLA Handbook (7^th Edition):

Hollenbach, Andrew. “Low-Cost Multiple-MAV SLAM Using Open Source Software.” 2018. Web. 11 Dec 2019.

Vancouver:

Hollenbach A. Low-Cost Multiple-MAV SLAM Using Open Source Software. [Internet] [Masters thesis]. Rochester Institute of Technology; 2018. [cited 2019 Dec 11]. Available from: https://scholarworks.rit.edu/theses/9861.

Council of Science Editors:

Hollenbach A. Low-Cost Multiple-MAV SLAM Using Open Source Software. [Masters Thesis]. Rochester Institute of Technology; 2018. Available from: https://scholarworks.rit.edu/theses/9861

Lehigh University

20. Rumbaugh, Jr., Douglas Bahr. A Design Proposal for a Novel Gun-Launched Unmanned Aerial System.

Degree: MS, Mechanical Engineering, 2018, Lehigh University

URL: https://preserve.lehigh.edu/etd/4318

► A proposed design for a gun-launched, unmanned aerial system (GLUAS) is presented, along with experimental data pertaining to the characterization of said design, and specifically… (more)

Subjects/Keywords: flexibility; MAV; steady flow; swept wing; UAS; UAV; Mechanical Engineering

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APA (6^th Edition):

Rumbaugh, Jr., D. B. (2018). A Design Proposal for a Novel Gun-Launched Unmanned Aerial System. (Thesis). Lehigh University. Retrieved from https://preserve.lehigh.edu/etd/4318

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

Chicago Manual of Style (16^th Edition):

Rumbaugh, Jr., Douglas Bahr. “A Design Proposal for a Novel Gun-Launched Unmanned Aerial System.” 2018. Thesis, Lehigh University. Accessed December 11, 2019. https://preserve.lehigh.edu/etd/4318.

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

MLA Handbook (7^th Edition):

Rumbaugh, Jr., Douglas Bahr. “A Design Proposal for a Novel Gun-Launched Unmanned Aerial System.” 2018. Web. 11 Dec 2019.

Vancouver:

Rumbaugh, Jr. DB. A Design Proposal for a Novel Gun-Launched Unmanned Aerial System. [Internet] [Thesis]. Lehigh University; 2018. [cited 2019 Dec 11]. Available from: https://preserve.lehigh.edu/etd/4318.

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

Council of Science Editors:

Rumbaugh, Jr. DB. A Design Proposal for a Novel Gun-Launched Unmanned Aerial System. [Thesis]. Lehigh University; 2018. Available from: https://preserve.lehigh.edu/etd/4318

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

Rochester Institute of Technology

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

Degree: Mechanical Engineering, 2011, Rochester Institute of Technology

URL: https://scholarworks.rit.edu/theses/5804

► 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 (6^th 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 (16^th Edition):

Prosser, Daniel. “Flapping wing design for a dragonfly-like micro air vehicle.” 2011. Thesis, Rochester Institute of Technology. Accessed December 11, 2019. 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 (7^th Edition):

Prosser, Daniel. “Flapping wing design for a dragonfly-like micro air vehicle.” 2011. Web. 11 Dec 2019.

Vancouver:

Prosser D. Flapping wing design for a dragonfly-like micro air vehicle. [Internet] [Thesis]. Rochester Institute of Technology; 2011. [cited 2019 Dec 11]. 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

University of Pennsylvania

22. Paulos, James John. Rotorcraft Blade Pitch Control Through Torque Modulation.

Degree: 2017, University of Pennsylvania

URL: https://repository.upenn.edu/edissertations/2901

► Micro air vehicle (MAV) technology has broken with simple mimicry of manned aircraft in order to fulfill emerging roles which demand low-cost reliability in the… (more)

▼ Micro air vehicle (MAV) technology has broken with simple mimicry of manned aircraft in order to fulfill emerging roles which demand low-cost reliability in the hands of novice users, safe operation in confined spaces, contact and manipulation of the environment, or merging vertical flight and forward flight capabilities. These specialized needs have motivated a surge of new specialized aircraft, but the majority of these design variations remain constrained by the same fundamental technologies underpinning their thrust and control. This dissertation solves the problem of simultaneously governing MAV thrust, roll, and pitch using only a single rotor and single motor. Such an actuator enables new cheap, robust, and light weight aircraft by eliminating the need for the complex ancillary controls of a conventional helicopter swashplate or the distributed propeller array of a quadrotor. An analytic model explains how cyclic blade pitch variations in a special passively articulated rotor may be obtained by modulating the main drive motor torque in phase with the rotor rotation. Experiments with rotors from 10 cm to 100 cm in diameter confirm the predicted blade lag, pitch, and flap motions. We show the operating principle scales similarly as traditional helicopter rotor technologies, but is subject to additional new dynamics and technology considerations. Using this new rotor, experimental aircraft from 29 g to 870 g demonstrate conventional flight capabilities without requiring more than two motors for actuation. In addition, we emulate the unusual capabilities of a fully actuated MAV over six degrees of freedom using only the thrust vectoring qualities of two teetering rotors. Such independent control over forces and moments has been previously obtained by holonomic or omnidirection multirotors with at least six motors, but we now demonstrate similar abilities using only two. Expressive control from a single actuator enables new categories of MAV, illustrated by experiments with a single actuator aircraft with spatial control and a vertical takeoff and landing airplane whose flight authority is derived entirely from two rotors.

Subjects/Keywords: dynamics; helicopter; MAV; robotics; swashplate; Aerospace Engineering; Robotics

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APA (6^th Edition):

Paulos, J. J. (2017). Rotorcraft Blade Pitch Control Through Torque Modulation. (Thesis). University of Pennsylvania. Retrieved from https://repository.upenn.edu/edissertations/2901

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

Chicago Manual of Style (16^th Edition):

Paulos, James John. “Rotorcraft Blade Pitch Control Through Torque Modulation.” 2017. Thesis, University of Pennsylvania. Accessed December 11, 2019. https://repository.upenn.edu/edissertations/2901.

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

MLA Handbook (7^th Edition):

Paulos, James John. “Rotorcraft Blade Pitch Control Through Torque Modulation.” 2017. Web. 11 Dec 2019.

Vancouver:

Paulos JJ. Rotorcraft Blade Pitch Control Through Torque Modulation. [Internet] [Thesis]. University of Pennsylvania; 2017. [cited 2019 Dec 11]. Available from: https://repository.upenn.edu/edissertations/2901.

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

Council of Science Editors:

Paulos JJ. Rotorcraft Blade Pitch Control Through Torque Modulation. [Thesis]. University of Pennsylvania; 2017. Available from: https://repository.upenn.edu/edissertations/2901

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

University of New South Wales

23. Watman, Daniel John. Analysis and optimisation of passive flapping wing propulsion for micro aerial vehicles.

Degree: Mechanical & Manufacturing Engineering, 2009, University of New South Wales

URL: http://handle.unsw.edu.au/1959.4/43715 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:5253/SOURCE02?view=true

► Flapping wing propulsion has the potential to revolutionise the field of Micro Aerial Vehicles (MAVs), but little is known about the effect of flapping motion… (more)

▼ Flapping wing propulsion has the potential to revolutionise the field of Micro Aerial Vehicles (MAVs), but little is known about the effect of flapping motion on the performance of flapping wings. Prototype MAVs have achieved flight with passive flapping wings moving in a sinusoidal flapping motion, but the possible benefits of alternative flapping motions have not been studied in detail.This thesis presents the development of an Integrated Testing System (ITS), which allows the evaluation of flapping wing performance for different flapping motions. A detailed parametric study of the effect of flapping motion on wing performance is performed, and the optimal flapping motion for several passive flapping wings is determined by hardware-in-the-loop optimisation of two wing performance metrics.The developed ITS was able to automatically test a variety of passive flapping wings, and demonstrated precise control of the flapping motion and accurate and repeatable measurements of average lift force, mechanical power, and wing twist angle. The parametric study revealed that of the three flapping motions tested, the sinusoidal flapping motion generated the highest lift force, but a smoothed triangular motion was able to generate lift significantly more efficiently under load. The optimal flapping motion was successfully determined for three flapping wings, and was found to increase the loaded efficiency of the wings by an average of 31% over a sinusoidal flapping motion. The determined optimal motion was almost identical for the three tested wings, and was found to strongly resemble the flapping motion of insectsThese findings demonstrate that significant improvements in the performance of passive flapping wings can be achieved by relatively minor variations of the flapping motion. This increased understanding will ideally lead to more efficient flapping wing MAVs with higher payloads, longer flight times, and improved performance. Advisors/Committee Members: Katupitiya, Jayantha, Mechanical & Manufacturing Engineering, Faculty of Engineering, UNSW, Furukawa, Tomonari, Virginia Tech.

Subjects/Keywords: optimisation; MAV; flapping wing

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APA (6^th Edition):

Watman, D. J. (2009). Analysis and optimisation of passive flapping wing propulsion for micro aerial vehicles. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/43715 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:5253/SOURCE02?view=true

Chicago Manual of Style (16^th Edition):

Watman, Daniel John. “Analysis and optimisation of passive flapping wing propulsion for micro aerial vehicles.” 2009. Doctoral Dissertation, University of New South Wales. Accessed December 11, 2019. http://handle.unsw.edu.au/1959.4/43715 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:5253/SOURCE02?view=true.

MLA Handbook (7^th Edition):

Watman, Daniel John. “Analysis and optimisation of passive flapping wing propulsion for micro aerial vehicles.” 2009. Web. 11 Dec 2019.

Vancouver:

Watman DJ. Analysis and optimisation of passive flapping wing propulsion for micro aerial vehicles. [Internet] [Doctoral dissertation]. University of New South Wales; 2009. [cited 2019 Dec 11]. Available from: http://handle.unsw.edu.au/1959.4/43715 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:5253/SOURCE02?view=true.

Council of Science Editors:

Watman DJ. Analysis and optimisation of passive flapping wing propulsion for micro aerial vehicles. [Doctoral Dissertation]. University of New South Wales; 2009. Available from: http://handle.unsw.edu.au/1959.4/43715 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:5253/SOURCE02?view=true

University of Pennsylvania

24. Liu, Sikang. Motion Planning For Micro Aerial Vehicles.

Degree: 2018, University of Pennsylvania

URL: https://repository.upenn.edu/edissertations/3146

► A Micro Aerial Vehicle (MAV) is capable of agile motion in 3D making it an ideal platform for developments of planning and control algorithms. For… (more)

Subjects/Keywords: Collision Avoidance; MAV; Motion Planning; Optimal Control; Quadrotor; Engineering; Robotics

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APA (6^th Edition):

Liu, S. (2018). Motion Planning For Micro Aerial Vehicles. (Thesis). University of Pennsylvania. Retrieved from https://repository.upenn.edu/edissertations/3146

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

Chicago Manual of Style (16^th Edition):

Liu, Sikang. “Motion Planning For Micro Aerial Vehicles.” 2018. Thesis, University of Pennsylvania. Accessed December 11, 2019. https://repository.upenn.edu/edissertations/3146.

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

MLA Handbook (7^th Edition):

Liu, Sikang. “Motion Planning For Micro Aerial Vehicles.” 2018. Web. 11 Dec 2019.

Vancouver:

Liu S. Motion Planning For Micro Aerial Vehicles. [Internet] [Thesis]. University of Pennsylvania; 2018. [cited 2019 Dec 11]. Available from: https://repository.upenn.edu/edissertations/3146.

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

Council of Science Editors:

Liu S. Motion Planning For Micro Aerial Vehicles. [Thesis]. University of Pennsylvania; 2018. Available from: https://repository.upenn.edu/edissertations/3146

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

Wright State University

25. Venugopal Chengappa, Bharath. A Study of Evolvable Hardware Adaptive Oscillators for Augmentation of Flapping-Wing Micro Air Vehicle Altitude Control.

Degree: MSCE, Computer Engineering, 2010, Wright State University

URL: http://rave.ohiolink.edu/etdc/view?acc_num=wright1278968118

► The control of insect-sized flapping-wing micro air vehicles is fraughtwith difficulties. Even when adequate control laws are known, limits oncomputational precision and floating-point processing can… (more)

Subjects/Keywords: Computer Science; Mutation Rate; FW-MAV; Minipop; Wing; Minipop Algorithm; e¿¿¿¿¿¿¿ects; Population Size

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

APA (6^th Edition):

Venugopal Chengappa, B. (2010). A Study of Evolvable Hardware Adaptive Oscillators for Augmentation of Flapping-Wing Micro Air Vehicle Altitude Control. (Masters Thesis). Wright State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=wright1278968118

Chicago Manual of Style (16^th Edition):

Venugopal Chengappa, Bharath. “A Study of Evolvable Hardware Adaptive Oscillators for Augmentation of Flapping-Wing Micro Air Vehicle Altitude Control.” 2010. Masters Thesis, Wright State University. Accessed December 11, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=wright1278968118.

MLA Handbook (7^th Edition):

Venugopal Chengappa, Bharath. “A Study of Evolvable Hardware Adaptive Oscillators for Augmentation of Flapping-Wing Micro Air Vehicle Altitude Control.” 2010. Web. 11 Dec 2019.

Vancouver:

Venugopal Chengappa B. A Study of Evolvable Hardware Adaptive Oscillators for Augmentation of Flapping-Wing Micro Air Vehicle Altitude Control. [Internet] [Masters thesis]. Wright State University; 2010. [cited 2019 Dec 11]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1278968118.

Council of Science Editors:

Venugopal Chengappa B. A Study of Evolvable Hardware Adaptive Oscillators for Augmentation of Flapping-Wing Micro Air Vehicle Altitude Control. [Masters Thesis]. Wright State University; 2010. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1278968118

RMIT University

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

Degree: 2013, RMIT University

URL: http://researchbank.rmit.edu.au/view/rmit:160502

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

APA (6^th 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 (16^th Edition):

Fisher, A. “The effect of freestream turbulence on fixed and flapping micro air vehicle wings.” 2013. Thesis, RMIT University. Accessed December 11, 2019. 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 (7^th Edition):

Fisher, A. “The effect of freestream turbulence on fixed and flapping micro air vehicle wings.” 2013. Web. 11 Dec 2019.

Vancouver:

Fisher A. The effect of freestream turbulence on fixed and flapping micro air vehicle wings. [Internet] [Thesis]. RMIT University; 2013. [cited 2019 Dec 11]. 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

27. Dousse, Nicolas. Aerial Human-Comfortable Collision-free Navigation in Dense Environments.

Degree: 2017, EPFL

URL: http://infoscience.epfl.ch/record/227320

► With current overuse of the road transportation system and planned increase in traffic, inno- vative solutions that overcome environmental and financial cost of the current… (more)

▼ With current overuse of the road transportation system and planned increase in traffic, inno- vative solutions that overcome environmental and financial cost of the current system should be assessed. A promising idea is the use of the third dimension for personal transportation. Therefore, the European project myCopter, funded under the 7th framework, aimed at en- abling the technologies for Personal Aerial Transportation Systems as breakthrough in 21st century transportation systems. This project was the starting point of this thesis. When multiple vehicles share a common part of the sky, the biggest challenge is the man- agement of the risk of collision. While optimal collision-free navigation strategies have been proposed for autonomous robots, trajectories and accelerations for Personal Aerial Vehicles (PAVs) should also take into account human comfort for their passengers, which has rarely been the focus of these studies. Comfort of the trajectories is a key factor in order for this new transportation mean to be accepted and adopted by everyday users. Existing strategies used to maximize human-comfort of trajectories are based on path planning strategies, which compute beforehand the whole trajectory, implementing comfort as an optimization criteria. Personal Aerial Transportation Systems will have a high density of vehicles, where the time to react to potential threats might decrease to a few seconds only. This might be insufficient to compute a new trajectory each time using these path planning strategies. Therefore, in this thesis, a reactive decentralized strategy is proposed, maximizing the comfort of the trajectories for humans traveling in a Personal Aerial Vehicle. To prove the feasibility of collision avoidance strategies, it is not sufficient anymore to validate them only in simulation, but, in addition, real-time tests in a realistic outdoor environment should be performed. Nowadays, single drones can be effectively controlled by a single operator on the ground. The challenge relies instead on an efficient management of a whole swarm of drone. In this thesis, a framework to perform outdoor drone experiment was developed in order to validate the proposed collision avoidance strategy. On the one hand, an autopilot framework was developed, tailored for multi-drone experiments, allowing fast and easy deployment and maintenance of a swarm of drones. On the other hand, a ground control interface is proposed in order to monitor, control and maintain safety in a flight with a swarm of drones. Using the autopilot framework together with the ground control interface, the proposed collision avoidance strategy was validated using 10 quadrotors flying autonomously outdoor in a challenging scenario. Advisors/Committee Members: Floreano, Dario.

Subjects/Keywords: Human-comfort; Collision-free navigation; Human-Swarm interface; Swarm experiments; UAV; Drones; MAV; Safety; Regulations

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APA (6^th Edition):

Dousse, N. (2017). Aerial Human-Comfortable Collision-free Navigation in Dense Environments. (Thesis). EPFL. Retrieved from http://infoscience.epfl.ch/record/227320

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

Chicago Manual of Style (16^th Edition):

Dousse, Nicolas. “Aerial Human-Comfortable Collision-free Navigation in Dense Environments.” 2017. Thesis, EPFL. Accessed December 11, 2019. http://infoscience.epfl.ch/record/227320.

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

MLA Handbook (7^th Edition):

Dousse, Nicolas. “Aerial Human-Comfortable Collision-free Navigation in Dense Environments.” 2017. Web. 11 Dec 2019.

Vancouver:

Dousse N. Aerial Human-Comfortable Collision-free Navigation in Dense Environments. [Internet] [Thesis]. EPFL; 2017. [cited 2019 Dec 11]. Available from: http://infoscience.epfl.ch/record/227320.

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

Council of Science Editors:

Dousse N. Aerial Human-Comfortable Collision-free Navigation in Dense Environments. [Thesis]. EPFL; 2017. Available from: http://infoscience.epfl.ch/record/227320

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

The Ohio State University

28. Mohan, Arvind Thanam. Data-Driven Analysis Methodologies for Unsteady Aerodynamics from High Fidelity Simulations.

Degree: PhD, Aero/Astro Engineering, 2017, The Ohio State University

URL: http://rave.ohiolink.edu/etdc/view?acc_num=osu1512058039822368

► Numerical methods and computational approaches for studying fluid flow have become increasingly popular and more mature in their capabilities since the 1960s, when the prohibitive… (more)

▼ Numerical methods and computational approaches for studying fluid flow have become increasingly popular and more mature in their capabilities since the 1960s, when the prohibitive experimental costs associated with flight vehicle development programs necessitated an alternative approach. Computational Fluid Dynamics (CFD) approaches for several practical applications were pioneered in the early 1980s, but despite the algorithmic advances the computing power necessary to compute full three-dimensional flow-fields remained a bottleneck. With the advent of powerful microprocessors and high performance supercomputers, high fidelity three-dimensional CFD for cases of practical interest have become feasible over the last couple of decades. Although these high fidelity simulations contain the desired physics, extracting that information is proving to be a challenge due to their extremely large size. For instance, a 3D Direct Numerical Simulation (DNS) or Large Eddy Simulation (LES) of an airfoil can produce terabytes of data. For such large datasets, it becomes difficult to use conventional analysis and visualization techniques without resorting to statistical methods more suited to such ``big data" problems. There are several such methods, each of which usually places emphasis on a certain aspect of the dataset. However, these can be used in conjunction with each other to complement each other to generate a comprehensive understanding of the fundamental physical mechanisms prevalent in a flow-field.The central goal of this dissertation is to develop strategies based on novel statistical, model reduction and signal processing techniques to derive such physical insights into large CFD datasets of practical interest. To demonstrate this, three high fidelity LES datasets of various unsteady flow-fields arising in Micro Air Vehicle (MAV) flight have been analyzed in depth. They are a) Static stall of a NACA 0015 airfoil with plasma control, b) Dynamic stall in a plunging SD 7003 airfoil, and c) Interaction of a stream-wise oriented vortex impinging on a rectangular wing, which is a canonical problem in the aerodynamics of formation flight. First, model reduction as an effective means to study complex, realistic flows is investigated. The recently popularized model reduction technique, Dynamic Mode Decomposition (DMD) has been given special emphasis in addition to the well known Proper Orthogonal Decomposition (POD), to study the three cases mentioned above. In the NACA 0015 static stall case, DMD analysis reveals a strong instability in the flow-field at a Strouhal number St = 2. Subsequent actuation with a Nano-Second Pulse Dielectric Barrier Discharge (NS-DBD) plasma actuator at this frequency is found to mitigate stall, indicating the effectiveness of DMD analysis in estimating actuation parameters for flow control a priori. The potential of DMD in understanding the physics of a turbulent flow-field is then further explored using the SD 7003 airfoil dynamic stall case. DMD shows that the large scale energetic structures in… Advisors/Committee Members: Gaitonde, Datta (Advisor).

Subjects/Keywords: Aerospace Engineering; CFD; aerodynamics; turbulence; DMD; EMD; Multivariate EMD; Matching Pursuits; Statistics; Wavelets; MAV; UAV

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APA (6^th Edition):

Mohan, A. T. (2017). Data-Driven Analysis Methodologies for Unsteady Aerodynamics from High Fidelity Simulations. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1512058039822368

Chicago Manual of Style (16^th Edition):

Mohan, Arvind Thanam. “Data-Driven Analysis Methodologies for Unsteady Aerodynamics from High Fidelity Simulations.” 2017. Doctoral Dissertation, The Ohio State University. Accessed December 11, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1512058039822368.

MLA Handbook (7^th Edition):

Mohan, Arvind Thanam. “Data-Driven Analysis Methodologies for Unsteady Aerodynamics from High Fidelity Simulations.” 2017. Web. 11 Dec 2019.

Vancouver:

Mohan AT. Data-Driven Analysis Methodologies for Unsteady Aerodynamics from High Fidelity Simulations. [Internet] [Doctoral dissertation]. The Ohio State University; 2017. [cited 2019 Dec 11]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1512058039822368.

Council of Science Editors:

Mohan AT. Data-Driven Analysis Methodologies for Unsteady Aerodynamics from High Fidelity Simulations. [Doctoral Dissertation]. The Ohio State University; 2017. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1512058039822368

29. Lu, Y. Structural Control Method Research motivated for MAV Lift Force Modification:.

Degree: 2013, Delft University of Technology

URL: http://resolver.tudelft.nl/uuid:9c9a5fea-940e-4ec4-9fb2-ccc28f1db919

► Micro Air Vehicle (MAV) is a group of unmanned aerial vehicles that is autonomous and with a size restriction. Thanks to its possible application ranging… (more)

Subjects/Keywords: FWMAV; MAV; actuator; shape modification

…States Defense Advanced Research Projects Agency has defined the term MAV as any flying vehicle… …high speed is needed for the vehicle to stay airborne at the MAV scale of dimensions, which… …wing vehicle, at the MAV scale of dimensions, the dominant force will be produced by friction… …change to downward direction. Therefore, the flapping-wing mechanism is chosen for the MAV in… …similar to the MAV and the insects are capable of hovering. It helps with the illustrations of…

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APA (6^th Edition):

Lu, Y. (2013). Structural Control Method Research motivated for MAV Lift Force Modification:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:9c9a5fea-940e-4ec4-9fb2-ccc28f1db919

Chicago Manual of Style (16^th Edition):

Lu, Y. “Structural Control Method Research motivated for MAV Lift Force Modification:.” 2013. Masters Thesis, Delft University of Technology. Accessed December 11, 2019. http://resolver.tudelft.nl/uuid:9c9a5fea-940e-4ec4-9fb2-ccc28f1db919.

MLA Handbook (7^th Edition):

Lu, Y. “Structural Control Method Research motivated for MAV Lift Force Modification:.” 2013. Web. 11 Dec 2019.

Vancouver:

Lu Y. Structural Control Method Research motivated for MAV Lift Force Modification:. [Internet] [Masters thesis]. Delft University of Technology; 2013. [cited 2019 Dec 11]. Available from: http://resolver.tudelft.nl/uuid:9c9a5fea-940e-4ec4-9fb2-ccc28f1db919.

Council of Science Editors:

Lu Y. Structural Control Method Research motivated for MAV Lift Force Modification:. [Masters Thesis]. Delft University of Technology; 2013. Available from: http://resolver.tudelft.nl/uuid:9c9a5fea-940e-4ec4-9fb2-ccc28f1db919

Mississippi State University

30. Walker, Calvin Russell. Development of a Proof-of-Concept Backpackable Unmanned Aerial Vehicle.

Degree: MS, Aerospace Engineering, 2006, Mississippi State University

URL: http://sun.library.msstate.edu/ETD-db/theses/available/etd-07072006-112057/ ;

► This thesis documents the design and development of a robust backpackable proof-of-concept unmanned aerial vehicle. The unmanned aerial vehicle?s design departs from existing configurations in… (more)

Subjects/Keywords: keel beam; unmanned; mav; backpackable; uav

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APA (6^th Edition):

Walker, C. R. (2006). Development of a Proof-of-Concept Backpackable Unmanned Aerial Vehicle. (Masters Thesis). Mississippi State University. Retrieved from http://sun.library.msstate.edu/ETD-db/theses/available/etd-07072006-112057/ ;

Chicago Manual of Style (16^th Edition):

Walker, Calvin Russell. “Development of a Proof-of-Concept Backpackable Unmanned Aerial Vehicle.” 2006. Masters Thesis, Mississippi State University. Accessed December 11, 2019. http://sun.library.msstate.edu/ETD-db/theses/available/etd-07072006-112057/ ;.

MLA Handbook (7^th Edition):

Walker, Calvin Russell. “Development of a Proof-of-Concept Backpackable Unmanned Aerial Vehicle.” 2006. Web. 11 Dec 2019.

Vancouver:

Walker CR. Development of a Proof-of-Concept Backpackable Unmanned Aerial Vehicle. [Internet] [Masters thesis]. Mississippi State University; 2006. [cited 2019 Dec 11]. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-07072006-112057/ ;.

Council of Science Editors:

Walker CR. Development of a Proof-of-Concept Backpackable Unmanned Aerial Vehicle. [Masters Thesis]. Mississippi State University; 2006. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-07072006-112057/ ;

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