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You searched for +publisher:"Georgia Tech" +contributor:("Costello, Mark"). Showing records 1 – 30 of 65 total matches.

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1. Beyer, Eric W. Design, testing, and performance of a hybrid micro vehicle - the Hopping Rotochute.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 A new hybrid micro vehicle, called the Hopping Rotochute, was developed to robustly explore environments with rough terrain while minimizing energy consumption over extended periods… (more)

Subjects/Keywords: Hopping; Micro air vehicle; Rotorcraft; Aerodynamics; Lifting bodies (Aeronautics) Flight testing; DYNAMO (Computer program language); Mobile robots; Robots

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APA (6th Edition):

Beyer, E. W. (2009). Design, testing, and performance of a hybrid micro vehicle - the Hopping Rotochute. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/29661

Chicago Manual of Style (16th Edition):

Beyer, Eric W. “Design, testing, and performance of a hybrid micro vehicle - the Hopping Rotochute.” 2009. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/29661.

MLA Handbook (7th Edition):

Beyer, Eric W. “Design, testing, and performance of a hybrid micro vehicle - the Hopping Rotochute.” 2009. Web. 20 Sep 2020.

Vancouver:

Beyer EW. Design, testing, and performance of a hybrid micro vehicle - the Hopping Rotochute. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/29661.

Council of Science Editors:

Beyer EW. Design, testing, and performance of a hybrid micro vehicle - the Hopping Rotochute. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/29661


Georgia Tech

2. Dowling, Matthew R. Energy harvesting for parafoil and payload aircraft systems.

Degree: MS, Mechanical Engineering, 2017, Georgia Tech

 Guided airdrop systems offer an efficient and reliable means of delivering payloads to remote or hard-to-access locations. Utilizing a set of sensors and actuators, the… (more)

Subjects/Keywords: Wind turbine; Wind energy; Guided airdrop systems

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APA (6th Edition):

Dowling, M. R. (2017). Energy harvesting for parafoil and payload aircraft systems. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59280

Chicago Manual of Style (16th Edition):

Dowling, Matthew R. “Energy harvesting for parafoil and payload aircraft systems.” 2017. Masters Thesis, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/59280.

MLA Handbook (7th Edition):

Dowling, Matthew R. “Energy harvesting for parafoil and payload aircraft systems.” 2017. Web. 20 Sep 2020.

Vancouver:

Dowling MR. Energy harvesting for parafoil and payload aircraft systems. [Internet] [Masters thesis]. Georgia Tech; 2017. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/59280.

Council of Science Editors:

Dowling MR. Energy harvesting for parafoil and payload aircraft systems. [Masters Thesis]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/59280


Georgia Tech

3. Choi, Su Yeon. Automatic mass balancing system for the 5-DOF spacecraft simulator.

Degree: MS, Aerospace Engineering, 2016, Georgia Tech

 Spacecraft simulators are widely used to validate spacecraft attitude determination and control techniques. The Autonomous Spacecraft Testing of Robotic Operations in Space (ASTROS) facility at… (more)

Subjects/Keywords: Balancing system; Control; PID; EKF; Spacecraft

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APA (6th Edition):

Choi, S. Y. (2016). Automatic mass balancing system for the 5-DOF spacecraft simulator. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55658

Chicago Manual of Style (16th Edition):

Choi, Su Yeon. “Automatic mass balancing system for the 5-DOF spacecraft simulator.” 2016. Masters Thesis, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/55658.

MLA Handbook (7th Edition):

Choi, Su Yeon. “Automatic mass balancing system for the 5-DOF spacecraft simulator.” 2016. Web. 20 Sep 2020.

Vancouver:

Choi SY. Automatic mass balancing system for the 5-DOF spacecraft simulator. [Internet] [Masters thesis]. Georgia Tech; 2016. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/55658.

Council of Science Editors:

Choi SY. Automatic mass balancing system for the 5-DOF spacecraft simulator. [Masters Thesis]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55658


Georgia Tech

4. Leonard, Andrew. Vehicle tracking using ultra-wideband radar.

Degree: MS, Mechanical Engineering, 2016, Georgia Tech

 In this thesis a vehicle tracking problem using an ultra-wideband radar sensor is considered. Prior research is heavily focused on specific applications, such as highway… (more)

Subjects/Keywords: Vehicle tracking; Ultra-wideband; Radar; Particle filter

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APA (6th Edition):

Leonard, A. (2016). Vehicle tracking using ultra-wideband radar. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/56265

Chicago Manual of Style (16th Edition):

Leonard, Andrew. “Vehicle tracking using ultra-wideband radar.” 2016. Masters Thesis, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/56265.

MLA Handbook (7th Edition):

Leonard, Andrew. “Vehicle tracking using ultra-wideband radar.” 2016. Web. 20 Sep 2020.

Vancouver:

Leonard A. Vehicle tracking using ultra-wideband radar. [Internet] [Masters thesis]. Georgia Tech; 2016. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/56265.

Council of Science Editors:

Leonard A. Vehicle tracking using ultra-wideband radar. [Masters Thesis]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/56265


Georgia Tech

5. Zhang, Xiaomo. Flight simulation and stability control of wingsuits.

Degree: MS, Aerospace Engineering, 2016, Georgia Tech

 Since French tailor Franz Reichelt made the earliest attempt in February 1912, wingsuits have been developed and widely used not only in extreme sports, but… (more)

Subjects/Keywords: Wingsuit; Simulation

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APA (6th Edition):

Zhang, X. (2016). Flight simulation and stability control of wingsuits. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/56290

Chicago Manual of Style (16th Edition):

Zhang, Xiaomo. “Flight simulation and stability control of wingsuits.” 2016. Masters Thesis, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/56290.

MLA Handbook (7th Edition):

Zhang, Xiaomo. “Flight simulation and stability control of wingsuits.” 2016. Web. 20 Sep 2020.

Vancouver:

Zhang X. Flight simulation and stability control of wingsuits. [Internet] [Masters thesis]. Georgia Tech; 2016. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/56290.

Council of Science Editors:

Zhang X. Flight simulation and stability control of wingsuits. [Masters Thesis]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/56290


Georgia Tech

6. Zhou, Min. Trajectory optimization for fuel cell powered UAVs.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 This dissertation progressively addresses research problems related to the trajectory optimization for fuel cell powered UAVs, from propulsion system model development, to optimal trajectory analyses… (more)

Subjects/Keywords: Trajectory optimization; Fuel cell powered UAVs; Route planning; Optimal control; Drone aircraft; Fuel cell vehicles; Systems engineering; Aeronautics Systems engineering; Trajectories (Mechanics)

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APA (6th Edition):

Zhou, M. (2013). Trajectory optimization for fuel cell powered UAVs. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/50235

Chicago Manual of Style (16th Edition):

Zhou, Min. “Trajectory optimization for fuel cell powered UAVs.” 2013. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/50235.

MLA Handbook (7th Edition):

Zhou, Min. “Trajectory optimization for fuel cell powered UAVs.” 2013. Web. 20 Sep 2020.

Vancouver:

Zhou M. Trajectory optimization for fuel cell powered UAVs. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/50235.

Council of Science Editors:

Zhou M. Trajectory optimization for fuel cell powered UAVs. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/50235


Georgia Tech

7. Potter, James Jackson. Input-shaped manual control of helicopters with suspended loads.

Degree: PhD, Mechanical Engineering, 2013, Georgia Tech

 A helicopter can be used to transport a load hanging from a suspension cable. This technique is frequently used in construction, firefighting, and disaster relief… (more)

Subjects/Keywords: Helicopter; Input shaping; Command filter; Sling load; Flexible system; Manual control; Human-in-the-loop control; Operator study; Handling qualities; Experimental platform; Dynamic modeling; Helicopters; Flight control; Cranes, derricks, etc. Dynamics; Feedback control systems; Damping (Mechanics)

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APA (6th Edition):

Potter, J. J. (2013). Input-shaped manual control of helicopters with suspended loads. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/50342

Chicago Manual of Style (16th Edition):

Potter, James Jackson. “Input-shaped manual control of helicopters with suspended loads.” 2013. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/50342.

MLA Handbook (7th Edition):

Potter, James Jackson. “Input-shaped manual control of helicopters with suspended loads.” 2013. Web. 20 Sep 2020.

Vancouver:

Potter JJ. Input-shaped manual control of helicopters with suspended loads. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/50342.

Council of Science Editors:

Potter JJ. Input-shaped manual control of helicopters with suspended loads. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/50342


Georgia Tech

8. Cook, James Richard. Development of an aeroelastic methodology for surface morphing rotors.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 A Computational Fluid Dynamics/Computational Fluid Dynamics (CFD/CSD) coupling interface was developed to obtain aeroelastic solutions of a morphing rotor. The methodology was implemented in Fully… (more)

Subjects/Keywords: Aeroelasticity; Test facility; Recirculation; Turbulence model; Hrles; Rotorcraft; Rotor; CFD/CSD; Coupling; CFD; Camber; Actuation; Morphing; Rotors; Aeroelasticity; Structural dynamics; Computational fluid dynamics

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APA (6th Edition):

Cook, J. R. (2014). Development of an aeroelastic methodology for surface morphing rotors. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/51807

Chicago Manual of Style (16th Edition):

Cook, James Richard. “Development of an aeroelastic methodology for surface morphing rotors.” 2014. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/51807.

MLA Handbook (7th Edition):

Cook, James Richard. “Development of an aeroelastic methodology for surface morphing rotors.” 2014. Web. 20 Sep 2020.

Vancouver:

Cook JR. Development of an aeroelastic methodology for surface morphing rotors. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/51807.

Council of Science Editors:

Cook JR. Development of an aeroelastic methodology for surface morphing rotors. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/51807


Georgia Tech

9. Gross, Matthew. Smart projectile parameter estimation using meta-optimization.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 System identification and parameter estimation are valuable tools in the analysis and design of smart projectile systems. Given the complexity of these systems, it is… (more)

Subjects/Keywords: Parameter estimation; Numerical optimization; Smart projectiles; Reinforcement learning

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APA (6th Edition):

Gross, M. (2017). Smart projectile parameter estimation using meta-optimization. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59190

Chicago Manual of Style (16th Edition):

Gross, Matthew. “Smart projectile parameter estimation using meta-optimization.” 2017. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/59190.

MLA Handbook (7th Edition):

Gross, Matthew. “Smart projectile parameter estimation using meta-optimization.” 2017. Web. 20 Sep 2020.

Vancouver:

Gross M. Smart projectile parameter estimation using meta-optimization. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/59190.

Council of Science Editors:

Gross M. Smart projectile parameter estimation using meta-optimization. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/59190


Georgia Tech

10. Schulte, Peter Z. A state machine architecture for aerospace vehicle fault protection.

Degree: PhD, Aerospace Engineering, 2018, Georgia Tech

 Because of their complexity and the unforgiving environment in which they operate, aerospace vehicles are vulnerable to mission-critical failures. In order to prevent these failures,… (more)

Subjects/Keywords: Fault protection; Fault detection, isolation, and recovery; Guidance, navigation, and control; State machines; On-board fault diagnosis; Aerospace systems engineering

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APA (6th Edition):

Schulte, P. Z. (2018). A state machine architecture for aerospace vehicle fault protection. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/60252

Chicago Manual of Style (16th Edition):

Schulte, Peter Z. “A state machine architecture for aerospace vehicle fault protection.” 2018. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/60252.

MLA Handbook (7th Edition):

Schulte, Peter Z. “A state machine architecture for aerospace vehicle fault protection.” 2018. Web. 20 Sep 2020.

Vancouver:

Schulte PZ. A state machine architecture for aerospace vehicle fault protection. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/60252.

Council of Science Editors:

Schulte PZ. A state machine architecture for aerospace vehicle fault protection. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/60252


Georgia Tech

11. Scheuermann, Edward J. Autonomous control of parafoil and payload systems using upper surface canopy spoilers.

Degree: PhD, Mechanical Engineering, 2015, Georgia Tech

 With the advent of steerable, ram air parafoil canopies, aerial payload delivery has become a viable alternative for situations involving remote or undeveloped areas, hostile… (more)

Subjects/Keywords: Airdrop systems; Autonomous control; Dynamic modeling; Guidance; Parachutes; Parafoils; Aerodynamic spoilers

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APA (6th Edition):

Scheuermann, E. J. (2015). Autonomous control of parafoil and payload systems using upper surface canopy spoilers. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53874

Chicago Manual of Style (16th Edition):

Scheuermann, Edward J. “Autonomous control of parafoil and payload systems using upper surface canopy spoilers.” 2015. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/53874.

MLA Handbook (7th Edition):

Scheuermann, Edward J. “Autonomous control of parafoil and payload systems using upper surface canopy spoilers.” 2015. Web. 20 Sep 2020.

Vancouver:

Scheuermann EJ. Autonomous control of parafoil and payload systems using upper surface canopy spoilers. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/53874.

Council of Science Editors:

Scheuermann EJ. Autonomous control of parafoil and payload systems using upper surface canopy spoilers. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/53874


Georgia Tech

12. Prosser, Daniel T. Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies.

Degree: PhD, Aerospace Engineering, 2015, Georgia Tech

 Interactions between the aerodynamics and dynamics of bluff bodies are important in many engineering applications, including suspension bridges, tall buildings, oil platforms, wind turbine towers,… (more)

Subjects/Keywords: Computational fluid dynamics; Reduced-order modeling; Tethered loads; Rotorcraft; Bluff bodies

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APA (6th Edition):

Prosser, D. T. (2015). Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53899

Chicago Manual of Style (16th Edition):

Prosser, Daniel T. “Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies.” 2015. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/53899.

MLA Handbook (7th Edition):

Prosser, Daniel T. “Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies.” 2015. Web. 20 Sep 2020.

Vancouver:

Prosser DT. Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/53899.

Council of Science Editors:

Prosser DT. Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/53899


Georgia Tech

13. Gissen, Abraham Naroll. Active flow control in high-speed internal flows.

Degree: PhD, Mechanical Engineering, 2015, Georgia Tech

 Manipulation of high-speed duct flow by streamwise vorticity concentration that are engendered by interactions of surface-mounted passive and active flow control actuators with the cross… (more)

Subjects/Keywords: Flow control shock

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APA (6th Edition):

Gissen, A. N. (2015). Active flow control in high-speed internal flows. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/54865

Chicago Manual of Style (16th Edition):

Gissen, Abraham Naroll. “Active flow control in high-speed internal flows.” 2015. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/54865.

MLA Handbook (7th Edition):

Gissen, Abraham Naroll. “Active flow control in high-speed internal flows.” 2015. Web. 20 Sep 2020.

Vancouver:

Gissen AN. Active flow control in high-speed internal flows. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/54865.

Council of Science Editors:

Gissen AN. Active flow control in high-speed internal flows. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/54865


Georgia Tech

14. DeSalvo, Michael E. Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control.

Degree: PhD, Mechanical Engineering, 2015, Georgia Tech

 The mechanisms of aerodynamic flow control over lifting surfaces in which global, large-scale changes in aerodynamic characteristics are engendered by momentum injection across the flow… (more)

Subjects/Keywords: Flow control; Aerodynamics

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APA (6th Edition):

DeSalvo, M. E. (2015). Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55498

Chicago Manual of Style (16th Edition):

DeSalvo, Michael E. “Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control.” 2015. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/55498.

MLA Handbook (7th Edition):

DeSalvo, Michael E. “Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control.” 2015. Web. 20 Sep 2020.

Vancouver:

DeSalvo ME. Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/55498.

Council of Science Editors:

DeSalvo ME. Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/55498


Georgia Tech

15. Kearney, John M. Aerodynamic control using distributed active bleed.

Degree: PhD, Mechanical Engineering, 2015, Georgia Tech

 A novel approach for controlling the global aerodynamic loads on lifting surfaces using regulated distributed active bleed that is driven by pressure differences across the… (more)

Subjects/Keywords: Fluid mechanics; Flow control

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APA (6th Edition):

Kearney, J. M. (2015). Aerodynamic control using distributed active bleed. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55515

Chicago Manual of Style (16th Edition):

Kearney, John M. “Aerodynamic control using distributed active bleed.” 2015. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/55515.

MLA Handbook (7th Edition):

Kearney, John M. “Aerodynamic control using distributed active bleed.” 2015. Web. 20 Sep 2020.

Vancouver:

Kearney JM. Aerodynamic control using distributed active bleed. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/55515.

Council of Science Editors:

Kearney JM. Aerodynamic control using distributed active bleed. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/55515


Georgia Tech

16. Cacan, Martin R. Adaptive control of autonomous airdrop systems in degraded conditions.

Degree: PhD, Mechanical Engineering, 2016, Georgia Tech

 Autonomous airdrop systems exhibit significant improvements over their unguided counterparts due to the addition of control mechanisms and real-time feedback. Increased landing accuracy comes with… (more)

Subjects/Keywords: Autonomous vehicles; Precision guided airdrop; Adaptive control

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APA (6th Edition):

Cacan, M. R. (2016). Adaptive control of autonomous airdrop systems in degraded conditions. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/56351

Chicago Manual of Style (16th Edition):

Cacan, Martin R. “Adaptive control of autonomous airdrop systems in degraded conditions.” 2016. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/56351.

MLA Handbook (7th Edition):

Cacan, Martin R. “Adaptive control of autonomous airdrop systems in degraded conditions.” 2016. Web. 20 Sep 2020.

Vancouver:

Cacan MR. Adaptive control of autonomous airdrop systems in degraded conditions. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/56351.

Council of Science Editors:

Cacan MR. Adaptive control of autonomous airdrop systems in degraded conditions. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/56351


Georgia Tech

17. Lambert, Thomas John. Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body.

Degree: PhD, Mechanical Engineering, 2016, Georgia Tech

 This research focuses on the unsteady flow mechanisms of using aerodynamic flow control at the aft end flow boundary of a bluff body to modify… (more)

Subjects/Keywords: Flow control; Fluid mechanics; Aerodynamics

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APA (6th Edition):

Lambert, T. J. (2016). Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/56356

Chicago Manual of Style (16th Edition):

Lambert, Thomas John. “Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body.” 2016. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/56356.

MLA Handbook (7th Edition):

Lambert, Thomas John. “Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body.” 2016. Web. 20 Sep 2020.

Vancouver:

Lambert TJ. Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/56356.

Council of Science Editors:

Lambert TJ. Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/56356


Georgia Tech

18. Magree, Daniel Paul. Monocular vision-aided inertial navigation for unmanned aerial vehicles.

Degree: PhD, Aerospace Engineering, 2015, Georgia Tech

 The reliance of unmanned aerial vehicles (UAVs) on GPS and other external navigation aids has become a limiting factor for many missions. UAVs are now… (more)

Subjects/Keywords: Visual navigation; Filtering; Extended Kalman filter; Factorization methods; Unmanned aerial vehicles

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APA (6th Edition):

Magree, D. P. (2015). Monocular vision-aided inertial navigation for unmanned aerial vehicles. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53892

Chicago Manual of Style (16th Edition):

Magree, Daniel Paul. “Monocular vision-aided inertial navigation for unmanned aerial vehicles.” 2015. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/53892.

MLA Handbook (7th Edition):

Magree, Daniel Paul. “Monocular vision-aided inertial navigation for unmanned aerial vehicles.” 2015. Web. 20 Sep 2020.

Vancouver:

Magree DP. Monocular vision-aided inertial navigation for unmanned aerial vehicles. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/53892.

Council of Science Editors:

Magree DP. Monocular vision-aided inertial navigation for unmanned aerial vehicles. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/53892

19. Adams, Christopher James. Modeling and control of helicopters carrying suspended loads.

Degree: MS, Mechanical Engineering, 2012, Georgia Tech

 Helicopters are often used to transport supplies and equipment. When a heavy load is carried via suspension cables below a helicopter, the load oscillates in… (more)

Subjects/Keywords: Model-following control; Input shaping; Modeling; Oscillations; Helicopters; Suspended loads; Helicopters; Cargo handling; Helicopters Control systems; Flight control; Feedback control systems

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APA (6th Edition):

Adams, C. J. (2012). Modeling and control of helicopters carrying suspended loads. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/44852

Chicago Manual of Style (16th Edition):

Adams, Christopher James. “Modeling and control of helicopters carrying suspended loads.” 2012. Masters Thesis, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/44852.

MLA Handbook (7th Edition):

Adams, Christopher James. “Modeling and control of helicopters carrying suspended loads.” 2012. Web. 20 Sep 2020.

Vancouver:

Adams CJ. Modeling and control of helicopters carrying suspended loads. [Internet] [Masters thesis]. Georgia Tech; 2012. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/44852.

Council of Science Editors:

Adams CJ. Modeling and control of helicopters carrying suspended loads. [Masters Thesis]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/44852

20. Ramaswamy, Nikhil. Development of control strategies to optimize the fuel economy of hybrid electric vehicles.

Degree: MS, Mechanical Engineering, 2014, Georgia Tech

 This thesis (1) reports a new Dynamic Programming (DP) approach, and (2) reports a Real Time Control strategy to optimize the energy management of a… (more)

Subjects/Keywords: Modeling and simulation; Control strategies; Hybrid electric vehicles; Hybrid electric cars; Dynamic programming; Control thoery

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APA (6th Edition):

Ramaswamy, N. (2014). Development of control strategies to optimize the fuel economy of hybrid electric vehicles. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/51887

Chicago Manual of Style (16th Edition):

Ramaswamy, Nikhil. “Development of control strategies to optimize the fuel economy of hybrid electric vehicles.” 2014. Masters Thesis, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/51887.

MLA Handbook (7th Edition):

Ramaswamy, Nikhil. “Development of control strategies to optimize the fuel economy of hybrid electric vehicles.” 2014. Web. 20 Sep 2020.

Vancouver:

Ramaswamy N. Development of control strategies to optimize the fuel economy of hybrid electric vehicles. [Internet] [Masters thesis]. Georgia Tech; 2014. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/51887.

Council of Science Editors:

Ramaswamy N. Development of control strategies to optimize the fuel economy of hybrid electric vehicles. [Masters Thesis]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/51887

21. Cole, Bjorn Forstrom. An evolutionary method for synthesizing technological planning and architectural advance.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 There are many times in which a critical choice between proposed system architectures must be made. Two situations in particular motivate this dissertation: a "Cambrian… (more)

Subjects/Keywords: Combinatorial optimization; Systems engineering; Strategic planning; Architecture; Genetic algorithms; Algorithms; Problem solving

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APA (6th Edition):

Cole, B. F. (2009). An evolutionary method for synthesizing technological planning and architectural advance. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/29758

Chicago Manual of Style (16th Edition):

Cole, Bjorn Forstrom. “An evolutionary method for synthesizing technological planning and architectural advance.” 2009. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/29758.

MLA Handbook (7th Edition):

Cole, Bjorn Forstrom. “An evolutionary method for synthesizing technological planning and architectural advance.” 2009. Web. 20 Sep 2020.

Vancouver:

Cole BF. An evolutionary method for synthesizing technological planning and architectural advance. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/29758.

Council of Science Editors:

Cole BF. An evolutionary method for synthesizing technological planning and architectural advance. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/29758

22. Noevere, August T. Rapid determination of mass and stiffness distribution on primary skin-stiffener structures.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 In modern conceptual/preliminary design of aerospace vehicles it is common for a large number of concepts and configurations to be rapidly explored. For each configuration,… (more)

Subjects/Keywords: Structural optimization; Stiffened panel optimization; Conceptual design

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APA (6th Edition):

Noevere, A. T. (2016). Rapid determination of mass and stiffness distribution on primary skin-stiffener structures. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55638

Chicago Manual of Style (16th Edition):

Noevere, August T. “Rapid determination of mass and stiffness distribution on primary skin-stiffener structures.” 2016. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/55638.

MLA Handbook (7th Edition):

Noevere, August T. “Rapid determination of mass and stiffness distribution on primary skin-stiffener structures.” 2016. Web. 20 Sep 2020.

Vancouver:

Noevere AT. Rapid determination of mass and stiffness distribution on primary skin-stiffener structures. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/55638.

Council of Science Editors:

Noevere AT. Rapid determination of mass and stiffness distribution on primary skin-stiffener structures. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55638

23. Wachlin, Jacob T. Computational improvements of a multibody dynamic simulation algorithm applied to a landing event simulation of a flexible legged Europa lander.

Degree: MS, Mechanical Engineering, 2018, Georgia Tech

 Multibody dynamic simulation is critical to the design and analysis of many mechanical systems. Engineers use these simulations to understand the motion and loading conditions… (more)

Subjects/Keywords: Multibody; Dynamic; Simulation; Constrained; Coordinate

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APA (6th Edition):

Wachlin, J. T. (2018). Computational improvements of a multibody dynamic simulation algorithm applied to a landing event simulation of a flexible legged Europa lander. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59964

Chicago Manual of Style (16th Edition):

Wachlin, Jacob T. “Computational improvements of a multibody dynamic simulation algorithm applied to a landing event simulation of a flexible legged Europa lander.” 2018. Masters Thesis, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/59964.

MLA Handbook (7th Edition):

Wachlin, Jacob T. “Computational improvements of a multibody dynamic simulation algorithm applied to a landing event simulation of a flexible legged Europa lander.” 2018. Web. 20 Sep 2020.

Vancouver:

Wachlin JT. Computational improvements of a multibody dynamic simulation algorithm applied to a landing event simulation of a flexible legged Europa lander. [Internet] [Masters thesis]. Georgia Tech; 2018. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/59964.

Council of Science Editors:

Wachlin JT. Computational improvements of a multibody dynamic simulation algorithm applied to a landing event simulation of a flexible legged Europa lander. [Masters Thesis]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/59964

24. Liggett, Nicholas Dwayne. Numerical investigation of static and dynamic stall of single and flapped airfoils.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 Separated flows about single and multi-element airfoils are featured in many scenarios of practical interest, including: stall of fixed wing aircraft, dynamic stall of rotorcraft… (more)

Subjects/Keywords: Separated flows; HRLES; LES; RANS; CFD; Stall; Separation; Turbulence; Numerical convergence; Oscillating airfoil; Multi-element airfoil; Stalling (Aerodynamics); Aerodynamics; Aerofoils

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APA (6th Edition):

Liggett, N. D. (2012). Numerical investigation of static and dynamic stall of single and flapped airfoils. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/45834

Chicago Manual of Style (16th Edition):

Liggett, Nicholas Dwayne. “Numerical investigation of static and dynamic stall of single and flapped airfoils.” 2012. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/45834.

MLA Handbook (7th Edition):

Liggett, Nicholas Dwayne. “Numerical investigation of static and dynamic stall of single and flapped airfoils.” 2012. Web. 20 Sep 2020.

Vancouver:

Liggett ND. Numerical investigation of static and dynamic stall of single and flapped airfoils. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/45834.

Council of Science Editors:

Liggett ND. Numerical investigation of static and dynamic stall of single and flapped airfoils. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/45834

25. Johnson, Kevin Lee. Prediction of operational envelope maneuverability effects on rotorcraft design.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 Military helicopter operations require precise maneuverability characteristics for performance to be determined for the entire helicopter flight envelope. Historically, these maneuverability analyses are combinatorial in… (more)

Subjects/Keywords: Flight mechanics; Dynamic simulation; Real-time analysis; Quantitative analysis; Data filtering; Maneuver taxonomy; Control independent simulation; Inverse simulation; Helicopters Control systems Design and construction; Flight control Design and construction; Trajectory optimization; Aerodynamics; Helicopters Aerodynamics

…Addressing the three major needs yielded a methodology termed GT-RISE, which stands for Georgia… …Tech Rotorcraft Inverse Simulation Environment. The methodology enables the impact of design… 

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APA (6th Edition):

Johnson, K. L. (2013). Prediction of operational envelope maneuverability effects on rotorcraft design. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/47601

Chicago Manual of Style (16th Edition):

Johnson, Kevin Lee. “Prediction of operational envelope maneuverability effects on rotorcraft design.” 2013. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/47601.

MLA Handbook (7th Edition):

Johnson, Kevin Lee. “Prediction of operational envelope maneuverability effects on rotorcraft design.” 2013. Web. 20 Sep 2020.

Vancouver:

Johnson KL. Prediction of operational envelope maneuverability effects on rotorcraft design. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/47601.

Council of Science Editors:

Johnson KL. Prediction of operational envelope maneuverability effects on rotorcraft design. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/47601

26. Shankare Gowda, Vrishank Raghav. Radial flow effects on a retreating rotor blade.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 This work studies the effects of radial flow on the aerodynamic phenomena occurring on a retreating blade with a focus on dynamic stall and reverse… (more)

Subjects/Keywords: Rotating blade; Dynamic stall; Radial flow; Reverse flow; Rotating disk; PIV; Instability; Vortex induced lift

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APA (6th Edition):

Shankare Gowda, V. R. (2014). Radial flow effects on a retreating rotor blade. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53403

Chicago Manual of Style (16th Edition):

Shankare Gowda, Vrishank Raghav. “Radial flow effects on a retreating rotor blade.” 2014. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/53403.

MLA Handbook (7th Edition):

Shankare Gowda, Vrishank Raghav. “Radial flow effects on a retreating rotor blade.” 2014. Web. 20 Sep 2020.

Vancouver:

Shankare Gowda VR. Radial flow effects on a retreating rotor blade. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/53403.

Council of Science Editors:

Shankare Gowda VR. Radial flow effects on a retreating rotor blade. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/53403

27. Zarovy, Samuel R. Improved gust rejection for a micro coaxial helicopter in urban environments.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 Due to their small size, relative covertness, and high maneuverability, micro rotorcraft are ideal for a plethora of civilian and military applications in an urban… (more)

Subjects/Keywords: Rotorcraft; Unmanned systems; Micro vehicles; ISR; Urban environments; Winds; Estimation; Modeling and simulation; Control

…Figure 2.8. Georgia Tech Indoor Flight Facility with VICON motion capture system. 24 Figure… 

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APA (6th Edition):

Zarovy, S. R. (2014). Improved gust rejection for a micro coaxial helicopter in urban environments. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/52992

Chicago Manual of Style (16th Edition):

Zarovy, Samuel R. “Improved gust rejection for a micro coaxial helicopter in urban environments.” 2014. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/52992.

MLA Handbook (7th Edition):

Zarovy, Samuel R. “Improved gust rejection for a micro coaxial helicopter in urban environments.” 2014. Web. 20 Sep 2020.

Vancouver:

Zarovy SR. Improved gust rejection for a micro coaxial helicopter in urban environments. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/52992.

Council of Science Editors:

Zarovy SR. Improved gust rejection for a micro coaxial helicopter in urban environments. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/52992

28. Reveles, Nicolas. Advanced methods for dynamic aeroelastic analysis of rotors.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 Simulations play an integral role in the understanding and development of rotor- craft aeromechanics. Computational Fluid Dynamics coupled with Computational Structural Dynamics (CFD/CSD) offers an… (more)

Subjects/Keywords: Aeroelasticity; Tight coupling; Loose coupling; CFD/CSD; Hybrid; Free-wake; URANS; Trim; Aeroelasticity; Rotors; Computational fluid dynamics; Structural dynamics

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APA (6th Edition):

Reveles, N. (2014). Advanced methods for dynamic aeroelastic analysis of rotors. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/51904

Chicago Manual of Style (16th Edition):

Reveles, Nicolas. “Advanced methods for dynamic aeroelastic analysis of rotors.” 2014. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/51904.

MLA Handbook (7th Edition):

Reveles, Nicolas. “Advanced methods for dynamic aeroelastic analysis of rotors.” 2014. Web. 20 Sep 2020.

Vancouver:

Reveles N. Advanced methods for dynamic aeroelastic analysis of rotors. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/51904.

Council of Science Editors:

Reveles N. Advanced methods for dynamic aeroelastic analysis of rotors. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/51904

29. Montalvo, Carlos. Meta aircraft flight dynamics and controls.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 The field of mobile robotic systems has become a rich area of research and design. These systems can navigate difficult terrain using multiple actuators with… (more)

Subjects/Keywords: Fixed wing aircraft; Flight dynamics; Drone aircraft; Reification; Multiagent systems; Aerodynamics; Flight control

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APA (6th Edition):

Montalvo, C. (2014). Meta aircraft flight dynamics and controls. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/51854

Chicago Manual of Style (16th Edition):

Montalvo, Carlos. “Meta aircraft flight dynamics and controls.” 2014. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/51854.

MLA Handbook (7th Edition):

Montalvo, Carlos. “Meta aircraft flight dynamics and controls.” 2014. Web. 20 Sep 2020.

Vancouver:

Montalvo C. Meta aircraft flight dynamics and controls. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/51854.

Council of Science Editors:

Montalvo C. Meta aircraft flight dynamics and controls. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/51854

30. Ward, Michael. Adaptive glide slope control for parafoil and payload aircraft.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 Airdrop systems provide a unique capability of delivering large payloads to undeveloped and inaccessible locations. Traditionally, these systems have been unguided, requiring large landing zones… (more)

Subjects/Keywords: Autonomous; Aircraft; Airdrop; Parafoil; Control; Parachutes; Glide path systems; Landing aids (Aeronautics); Payloads (Aerospace engineering)

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APA (6th Edition):

Ward, M. (2012). Adaptive glide slope control for parafoil and payload aircraft. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/44710

Chicago Manual of Style (16th Edition):

Ward, Michael. “Adaptive glide slope control for parafoil and payload aircraft.” 2012. Doctoral Dissertation, Georgia Tech. Accessed September 20, 2020. http://hdl.handle.net/1853/44710.

MLA Handbook (7th Edition):

Ward, Michael. “Adaptive glide slope control for parafoil and payload aircraft.” 2012. Web. 20 Sep 2020.

Vancouver:

Ward M. Adaptive glide slope control for parafoil and payload aircraft. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2020 Sep 20]. Available from: http://hdl.handle.net/1853/44710.

Council of Science Editors:

Ward M. Adaptive glide slope control for parafoil and payload aircraft. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/44710

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