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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 April 18, 2019. 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. 18 Apr 2019.

Vancouver:

Beyer EW. Design, testing, and performance of a hybrid micro vehicle - the Hopping Rotochute. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2019 Apr 18]. 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. 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 April 18, 2019. 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. 18 Apr 2019.

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 2019 Apr 18]. 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


Georgia Tech

3. 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 April 18, 2019. http://hdl.handle.net/1853/56265.

MLA Handbook (7th Edition):

Leonard, Andrew. “Vehicle tracking using ultra-wideband radar.” 2016. Web. 18 Apr 2019.

Vancouver:

Leonard A. Vehicle tracking using ultra-wideband radar. [Internet] [Masters thesis]. Georgia Tech; 2016. [cited 2019 Apr 18]. 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

4. 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 April 18, 2019. 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. 18 Apr 2019.

Vancouver:

Noevere AT. Rapid determination of mass and stiffness distribution on primary skin-stiffener structures. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Apr 18]. 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


Georgia Tech

5. 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 April 18, 2019. 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. 18 Apr 2019.

Vancouver:

Choi SY. Automatic mass balancing system for the 5-DOF spacecraft simulator. [Internet] [Masters thesis]. Georgia Tech; 2016. [cited 2019 Apr 18]. 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

6. 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 April 18, 2019. http://hdl.handle.net/1853/56290.

MLA Handbook (7th Edition):

Zhang, Xiaomo. “Flight simulation and stability control of wingsuits.” 2016. Web. 18 Apr 2019.

Vancouver:

Zhang X. Flight simulation and stability control of wingsuits. [Internet] [Masters thesis]. Georgia Tech; 2016. [cited 2019 Apr 18]. 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

7. Hart, Peter Bartholomew. A plm implementation for aerospace systems engineering-conceptual rotorcraft design.

Degree: MS, Aerospace Engineering, 2009, Georgia Tech

 The thesis will discuss the Systems Engineering phase of an original Conceptual Design Engineering Methodology for Aerospace Engineering-Vehicle Synthesis. This iterative phase is shown to… (more)

Subjects/Keywords: Teamcenter systems engineering; Teamcenter community; Teamcenter unified; Teamcenter engineering; Teamcenter manufacturing; CATIA V5; Rotorcraft design; Boeing; AHS; Joint heavy lift; VPLM; MBOM; EBOM; Product change control; Product definition; Configuration management; Product structure architecture; Design engineering; Aerospace engineering; System engineering; PLM; CIE; IDE; SE; Affordability; Cost savings; Executive helicopter; Joint chiefs of staff; Marine; CAE; CAD; CAM; CAA; MDO; RSM; DOE; Consulting; Engineering management; Perfect storm; Engineering software; Requirements data management; CATIA V4; NX; Engineering communications; RFP; Digitization; Air Force; Navy; Army; BAMS; FIPER; ACSYNT; Sikorsky; Bell; Georgia Tech; Engineering methodology; Requirements engineering; System engineering; Business process re-engineering conceptual design; Search; Rescue; IDE; Integrated digital environment; Kingfisher; Search and rescue; Helicopter; Helicopter engineering; QFD; Legacy design; IPPD; Quality engineering; Defense systems acquisition; Coast Guard; Decision support systems; Rotors (Helicopters) Design; Concurrent engineering

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APA (6th Edition):

Hart, P. B. (2009). A plm implementation for aerospace systems engineering-conceptual rotorcraft design. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/28278

Chicago Manual of Style (16th Edition):

Hart, Peter Bartholomew. “A plm implementation for aerospace systems engineering-conceptual rotorcraft design.” 2009. Masters Thesis, Georgia Tech. Accessed April 18, 2019. http://hdl.handle.net/1853/28278.

MLA Handbook (7th Edition):

Hart, Peter Bartholomew. “A plm implementation for aerospace systems engineering-conceptual rotorcraft design.” 2009. Web. 18 Apr 2019.

Vancouver:

Hart PB. A plm implementation for aerospace systems engineering-conceptual rotorcraft design. [Internet] [Masters thesis]. Georgia Tech; 2009. [cited 2019 Apr 18]. Available from: http://hdl.handle.net/1853/28278.

Council of Science Editors:

Hart PB. A plm implementation for aerospace systems engineering-conceptual rotorcraft design. [Masters Thesis]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/28278


Georgia Tech

8. Kim, Dooroo. Dynamic modeling of belt drives using the elastic/perfectly-plastic friction law.

Degree: MS, Mechanical Engineering, 2009, Georgia Tech

 Belt drives are used in numerous applications to transmit power between various machine elements. One limitation of the use of belt drives is the poor… (more)

Subjects/Keywords: Belt drives; Friction; Belt drives; Sliding friction; Mathematical models

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APA (6th Edition):

Kim, D. (2009). Dynamic modeling of belt drives using the elastic/perfectly-plastic friction law. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/29637

Chicago Manual of Style (16th Edition):

Kim, Dooroo. “Dynamic modeling of belt drives using the elastic/perfectly-plastic friction law.” 2009. Masters Thesis, Georgia Tech. Accessed April 18, 2019. http://hdl.handle.net/1853/29637.

MLA Handbook (7th Edition):

Kim, Dooroo. “Dynamic modeling of belt drives using the elastic/perfectly-plastic friction law.” 2009. Web. 18 Apr 2019.

Vancouver:

Kim D. Dynamic modeling of belt drives using the elastic/perfectly-plastic friction law. [Internet] [Masters thesis]. Georgia Tech; 2009. [cited 2019 Apr 18]. Available from: http://hdl.handle.net/1853/29637.

Council of Science Editors:

Kim D. Dynamic modeling of belt drives using the elastic/perfectly-plastic friction law. [Masters Thesis]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/29637


Georgia Tech

9. Clark, Brian. Modeling dynamic stall of SC-1095 airfoil at high mach number.

Degree: MS, Aerospace Engineering, 2010, Georgia Tech

 In this thesis, the Leishman-Beddoes method of determining airloads for an airfoil undergoing dynamic stall is studied over a range of Mach numbers. To validate… (more)

Subjects/Keywords: Dynamic stall; Leishman-Beddoes; Mach number; Aerofoils; Stalling (Aerodynamics)

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APA (6th Edition):

Clark, B. (2010). Modeling dynamic stall of SC-1095 airfoil at high mach number. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/33866

Chicago Manual of Style (16th Edition):

Clark, Brian. “Modeling dynamic stall of SC-1095 airfoil at high mach number.” 2010. Masters Thesis, Georgia Tech. Accessed April 18, 2019. http://hdl.handle.net/1853/33866.

MLA Handbook (7th Edition):

Clark, Brian. “Modeling dynamic stall of SC-1095 airfoil at high mach number.” 2010. Web. 18 Apr 2019.

Vancouver:

Clark B. Modeling dynamic stall of SC-1095 airfoil at high mach number. [Internet] [Masters thesis]. Georgia Tech; 2010. [cited 2019 Apr 18]. Available from: http://hdl.handle.net/1853/33866.

Council of Science Editors:

Clark B. Modeling dynamic stall of SC-1095 airfoil at high mach number. [Masters Thesis]. Georgia Tech; 2010. Available from: http://hdl.handle.net/1853/33866


Georgia Tech

10. Maleki, Ehsan A. Dynamics and control of a small-scale mobile boom crane.

Degree: MS, Mechanical Engineering, 2010, Georgia Tech

 Boom cranes are one of the most dynamically complicated types of cranes because they possess rotational joints as opposed to the linear tracks of bridge… (more)

Subjects/Keywords: Open-loop control; Flexible systems; Robotics; Modeling; Nonlinear dynamics; Cranes, derricks, etc.; Mobile cranes; Oscillations

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APA (6th Edition):

Maleki, E. A. (2010). Dynamics and control of a small-scale mobile boom crane. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/37166

Chicago Manual of Style (16th Edition):

Maleki, Ehsan A. “Dynamics and control of a small-scale mobile boom crane.” 2010. Masters Thesis, Georgia Tech. Accessed April 18, 2019. http://hdl.handle.net/1853/37166.

MLA Handbook (7th Edition):

Maleki, Ehsan A. “Dynamics and control of a small-scale mobile boom crane.” 2010. Web. 18 Apr 2019.

Vancouver:

Maleki EA. Dynamics and control of a small-scale mobile boom crane. [Internet] [Masters thesis]. Georgia Tech; 2010. [cited 2019 Apr 18]. Available from: http://hdl.handle.net/1853/37166.

Council of Science Editors:

Maleki EA. Dynamics and control of a small-scale mobile boom crane. [Masters Thesis]. Georgia Tech; 2010. Available from: http://hdl.handle.net/1853/37166


Georgia Tech

11. 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 April 18, 2019. http://hdl.handle.net/1853/59280.

MLA Handbook (7th Edition):

Dowling, Matthew R. “Energy harvesting for parafoil and payload aircraft systems.” 2017. Web. 18 Apr 2019.

Vancouver:

Dowling MR. Energy harvesting for parafoil and payload aircraft systems. [Internet] [Masters thesis]. Georgia Tech; 2017. [cited 2019 Apr 18]. 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

12. 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 April 18, 2019. http://hdl.handle.net/1853/50235.

MLA Handbook (7th Edition):

Zhou, Min. “Trajectory optimization for fuel cell powered UAVs.” 2013. Web. 18 Apr 2019.

Vancouver:

Zhou M. Trajectory optimization for fuel cell powered UAVs. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2019 Apr 18]. 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

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 April 18, 2019. http://hdl.handle.net/1853/54865.

MLA Handbook (7th Edition):

Gissen, Abraham Naroll. “Active flow control in high-speed internal flows.” 2015. Web. 18 Apr 2019.

Vancouver:

Gissen AN. Active flow control in high-speed internal flows. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Apr 18]. 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. 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 April 18, 2019. http://hdl.handle.net/1853/50342.

MLA Handbook (7th Edition):

Potter, James Jackson. “Input-shaped manual control of helicopters with suspended loads.” 2013. Web. 18 Apr 2019.

Vancouver:

Potter JJ. Input-shaped manual control of helicopters with suspended loads. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2019 Apr 18]. 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

15. 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 April 18, 2019. http://hdl.handle.net/1853/51807.

MLA Handbook (7th Edition):

Cook, James Richard. “Development of an aeroelastic methodology for surface morphing rotors.” 2014. Web. 18 Apr 2019.

Vancouver:

Cook JR. Development of an aeroelastic methodology for surface morphing rotors. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Apr 18]. 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

16. 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 April 18, 2019. 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. 18 Apr 2019.

Vancouver:

Scheuermann EJ. Autonomous control of parafoil and payload systems using upper surface canopy spoilers. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Apr 18]. 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

17. 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 April 18, 2019. 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. 18 Apr 2019.

Vancouver:

Prosser DT. Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Apr 18]. 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

18. 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 April 18, 2019. http://hdl.handle.net/1853/56351.

MLA Handbook (7th Edition):

Cacan, Martin R. “Adaptive control of autonomous airdrop systems in degraded conditions.” 2016. Web. 18 Apr 2019.

Vancouver:

Cacan MR. Adaptive control of autonomous airdrop systems in degraded conditions. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Apr 18]. 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

19. 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 April 18, 2019. 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. 18 Apr 2019.

Vancouver:

Lambert TJ. Aerodynamic control of flow dynamics coupled to a free-flight axisymmetric body. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Apr 18]. 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

20. Rajmohan, Nischint. Application of hybrid methodology to rotors in steady and maneuvering flight.

Degree: PhD, Aerospace Engineering, 2010, Georgia Tech

 Helicopters are versatile flying machines that have capabilities that are unparalleled by fixed wing aircraft, such as operating in hover, performing vertical take-off and landing… (more)

Subjects/Keywords: Aeroelasticity; Rotorcraft; CFD; Helicopters; Helicopters Aerodynamics; Vibration (Aeronautics) Damping; Computational fluid dynamics

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APA (6th Edition):

Rajmohan, N. (2010). Application of hybrid methodology to rotors in steady and maneuvering flight. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/34756

Chicago Manual of Style (16th Edition):

Rajmohan, Nischint. “Application of hybrid methodology to rotors in steady and maneuvering flight.” 2010. Doctoral Dissertation, Georgia Tech. Accessed April 18, 2019. http://hdl.handle.net/1853/34756.

MLA Handbook (7th Edition):

Rajmohan, Nischint. “Application of hybrid methodology to rotors in steady and maneuvering flight.” 2010. Web. 18 Apr 2019.

Vancouver:

Rajmohan N. Application of hybrid methodology to rotors in steady and maneuvering flight. [Internet] [Doctoral dissertation]. Georgia Tech; 2010. [cited 2019 Apr 18]. Available from: http://hdl.handle.net/1853/34756.

Council of Science Editors:

Rajmohan N. Application of hybrid methodology to rotors in steady and maneuvering flight. [Doctoral Dissertation]. Georgia Tech; 2010. Available from: http://hdl.handle.net/1853/34756


Georgia Tech

21. Tangen, Steven Anthony. A methodology for the quantification of doctrine and materiel approaches in a capability-based assessment.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 Due to the complexities of modern military operations and the technologies employed on today's military systems, acquisition costs and development times are becoming increasingly large.… (more)

Subjects/Keywords: Aerospace engineering; Doctrine; JCIDS; Unmanned aircraft; Defense acquisition; Operational readiness (Military science) Analysis; Technology Design

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APA (6th Edition):

Tangen, S. A. (2009). A methodology for the quantification of doctrine and materiel approaches in a capability-based assessment. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/28105

Chicago Manual of Style (16th Edition):

Tangen, Steven Anthony. “A methodology for the quantification of doctrine and materiel approaches in a capability-based assessment.” 2009. Doctoral Dissertation, Georgia Tech. Accessed April 18, 2019. http://hdl.handle.net/1853/28105.

MLA Handbook (7th Edition):

Tangen, Steven Anthony. “A methodology for the quantification of doctrine and materiel approaches in a capability-based assessment.” 2009. Web. 18 Apr 2019.

Vancouver:

Tangen SA. A methodology for the quantification of doctrine and materiel approaches in a capability-based assessment. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2019 Apr 18]. Available from: http://hdl.handle.net/1853/28105.

Council of Science Editors:

Tangen SA. A methodology for the quantification of doctrine and materiel approaches in a capability-based assessment. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/28105


Georgia Tech

22. Abras, Jennifer N. Enhancement of aeroelastic rotor airload prediction methods.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 The accurate prediction of rotor air loads is a current topic of interest in the rotorcraft community. The complex nature of this loading makes this… (more)

Subjects/Keywords: Coupling; CFD-CSD; Comprehensive code; Free wake; CFD; Rotor; Aeroelasticity; Rotors (Helicopters) Aerodynamics; Structural dynamics; Prediction theory

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APA (6th Edition):

Abras, J. N. (2009). Enhancement of aeroelastic rotor airload prediction methods. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/28182

Chicago Manual of Style (16th Edition):

Abras, Jennifer N. “Enhancement of aeroelastic rotor airload prediction methods.” 2009. Doctoral Dissertation, Georgia Tech. Accessed April 18, 2019. http://hdl.handle.net/1853/28182.

MLA Handbook (7th Edition):

Abras, Jennifer N. “Enhancement of aeroelastic rotor airload prediction methods.” 2009. Web. 18 Apr 2019.

Vancouver:

Abras JN. Enhancement of aeroelastic rotor airload prediction methods. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2019 Apr 18]. Available from: http://hdl.handle.net/1853/28182.

Council of Science Editors:

Abras JN. Enhancement of aeroelastic rotor airload prediction methods. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/28182


Georgia Tech

23. Moon, Jongki. Mission-based guidance system design for autonomous UAVs.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 The advantages of UAVs in the aviation arena have led to extensive research activities on autonomous technology of UAVs to achieve specific mission objectives. This… (more)

Subjects/Keywords: Obstacle avoidance; Envelope protection; Adptive control; Optimal control; NTG; UAV; Formation flight; Drone aircraft Control systems; Drone aircraft; Guidance systems (Flight)

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APA (6th Edition):

Moon, J. (2009). Mission-based guidance system design for autonomous UAVs. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/31797

Chicago Manual of Style (16th Edition):

Moon, Jongki. “Mission-based guidance system design for autonomous UAVs.” 2009. Doctoral Dissertation, Georgia Tech. Accessed April 18, 2019. http://hdl.handle.net/1853/31797.

MLA Handbook (7th Edition):

Moon, Jongki. “Mission-based guidance system design for autonomous UAVs.” 2009. Web. 18 Apr 2019.

Vancouver:

Moon J. Mission-based guidance system design for autonomous UAVs. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2019 Apr 18]. Available from: http://hdl.handle.net/1853/31797.

Council of Science Editors:

Moon J. Mission-based guidance system design for autonomous UAVs. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/31797


Georgia Tech

24. Gündüz, Mustafa Emre. Software integration for automated stability analysis and design optimization of a bearingless rotor blade.

Degree: PhD, Aerospace Engineering, 2010, Georgia Tech

 The concept of applying several disciplines to the design and optimization processes may not be new, but it does not currently seem to be widely… (more)

Subjects/Keywords: Design optimization; Software integration; CAD; Multidisciplinary; Vibration; Bearingless rotor; Rotors (Helicopters); Rotors (Helicopters)Design; Vibration (Aeronautics)

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APA (6th Edition):

Gündüz, M. E. (2010). Software integration for automated stability analysis and design optimization of a bearingless rotor blade. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/33916

Chicago Manual of Style (16th Edition):

Gündüz, Mustafa Emre. “Software integration for automated stability analysis and design optimization of a bearingless rotor blade.” 2010. Doctoral Dissertation, Georgia Tech. Accessed April 18, 2019. http://hdl.handle.net/1853/33916.

MLA Handbook (7th Edition):

Gündüz, Mustafa Emre. “Software integration for automated stability analysis and design optimization of a bearingless rotor blade.” 2010. Web. 18 Apr 2019.

Vancouver:

Gündüz ME. Software integration for automated stability analysis and design optimization of a bearingless rotor blade. [Internet] [Doctoral dissertation]. Georgia Tech; 2010. [cited 2019 Apr 18]. Available from: http://hdl.handle.net/1853/33916.

Council of Science Editors:

Gündüz ME. Software integration for automated stability analysis and design optimization of a bearingless rotor blade. [Doctoral Dissertation]. Georgia Tech; 2010. Available from: http://hdl.handle.net/1853/33916


Georgia Tech

25. Sobers, David Michael, Jr. Efficient ranging-sensor navigation methods for indoor aircraft.

Degree: PhD, Aerospace Engineering, 2010, Georgia Tech

 Unmanned Aerial Vehicles are often used for reconnaissance, search and rescue, damage assessment, exploration, and other tasks that are dangerous or prohibitively difficult for humans… (more)

Subjects/Keywords: Rotorcraft; Sensor; Dilution; Helicopter; Precision; Scanner; Wall; Obstacle; Flight; Coaxial; Quadrotor; Stabilization; Indoor; Sonar; Mapping; UAV; MAV; Autonomous; Aircraft; Guidance; Navigation; Control; Indoor; Laser; Inertial; SLAM; Localization; Infrared; Detectors; Stability of helicopters; Aerodynamics; Proximity detectors

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APA (6th Edition):

Sobers, David Michael, J. (2010). Efficient ranging-sensor navigation methods for indoor aircraft. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/34824

Chicago Manual of Style (16th Edition):

Sobers, David Michael, Jr. “Efficient ranging-sensor navigation methods for indoor aircraft.” 2010. Doctoral Dissertation, Georgia Tech. Accessed April 18, 2019. http://hdl.handle.net/1853/34824.

MLA Handbook (7th Edition):

Sobers, David Michael, Jr. “Efficient ranging-sensor navigation methods for indoor aircraft.” 2010. Web. 18 Apr 2019.

Vancouver:

Sobers, David Michael J. Efficient ranging-sensor navigation methods for indoor aircraft. [Internet] [Doctoral dissertation]. Georgia Tech; 2010. [cited 2019 Apr 18]. Available from: http://hdl.handle.net/1853/34824.

Council of Science Editors:

Sobers, David Michael J. Efficient ranging-sensor navigation methods for indoor aircraft. [Doctoral Dissertation]. Georgia Tech; 2010. Available from: http://hdl.handle.net/1853/34824


Georgia Tech

26. 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 April 18, 2019. 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. 18 Apr 2019.

Vancouver:

DeSalvo ME. Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Apr 18]. 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

27. 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 April 18, 2019. http://hdl.handle.net/1853/55515.

MLA Handbook (7th Edition):

Kearney, John M. “Aerodynamic control using distributed active bleed.” 2015. Web. 18 Apr 2019.

Vancouver:

Kearney JM. Aerodynamic control using distributed active bleed. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Apr 18]. 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

28. 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 April 18, 2019. http://hdl.handle.net/1853/59190.

MLA Handbook (7th Edition):

Gross, Matthew. “Smart projectile parameter estimation using meta-optimization.” 2017. Web. 18 Apr 2019.

Vancouver:

Gross M. Smart projectile parameter estimation using meta-optimization. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2019 Apr 18]. 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

29. 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 April 18, 2019. http://hdl.handle.net/1853/60252.

MLA Handbook (7th Edition):

Schulte, Peter Z. “A state machine architecture for aerospace vehicle fault protection.” 2018. Web. 18 Apr 2019.

Vancouver:

Schulte PZ. A state machine architecture for aerospace vehicle fault protection. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2019 Apr 18]. 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

30. 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 April 18, 2019. http://hdl.handle.net/1853/53892.

MLA Handbook (7th Edition):

Magree, Daniel Paul. “Monocular vision-aided inertial navigation for unmanned aerial vehicles.” 2015. Web. 18 Apr 2019.

Vancouver:

Magree DP. Monocular vision-aided inertial navigation for unmanned aerial vehicles. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Apr 18]. 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

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