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You searched for +publisher:"University of Florida" +contributor:("Lind, Richard C."). Showing records 1 – 30 of 34 total matches.

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University of Florida

1. Sorley, Stephen. Identification and Analysis of Time-Varying Modal Parameters.

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

 In this thesis, methods for identifying and analyzing the modal parameters of a linear, time-varying system with no control input are proposed. These methods are… (more)

Subjects/Keywords: Aircraft; Cost functions; Eigenvectors; Labor theories of value; Mathematical vectors; Matrices; Modal response; Scalars; State vectors; Trajectories; aircraft, control, eigenvalue, identification, kamen, mode, morphing, pole, time, varying

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APA (6th Edition):

Sorley, S. (2010). Identification and Analysis of Time-Varying Modal Parameters. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0042601

Chicago Manual of Style (16th Edition):

Sorley, Stephen. “Identification and Analysis of Time-Varying Modal Parameters.” 2010. Masters Thesis, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0042601.

MLA Handbook (7th Edition):

Sorley, Stephen. “Identification and Analysis of Time-Varying Modal Parameters.” 2010. Web. 16 Sep 2019.

Vancouver:

Sorley S. Identification and Analysis of Time-Varying Modal Parameters. [Internet] [Masters thesis]. University of Florida; 2010. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0042601.

Council of Science Editors:

Sorley S. Identification and Analysis of Time-Varying Modal Parameters. [Masters Thesis]. University of Florida; 2010. Available from: http://ufdc.ufl.edu/UFE0042601


University of Florida

2. Oh, Sang Min. Modeling and Control of a Quad-Rotor Helicopter.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2012, University of Florida

 The quad-rotor helicopter is a UAV (Un-manned Air Vehicle) and has four rotors. To get efficient stabilization status, the author applied PD (Proportional, Derivative) and… (more)

Subjects/Keywords: Block diagrams; Helicopters; Hovering; Hubs; Mathematical integrals; Mathematical robustness; Modeling; Moments of inertia; Simulations; Yaw rotation; controller  – pd  – pid  – quadrotor

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APA (6th Edition):

Oh, S. M. (2012). Modeling and Control of a Quad-Rotor Helicopter. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0044145

Chicago Manual of Style (16th Edition):

Oh, Sang Min. “Modeling and Control of a Quad-Rotor Helicopter.” 2012. Masters Thesis, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0044145.

MLA Handbook (7th Edition):

Oh, Sang Min. “Modeling and Control of a Quad-Rotor Helicopter.” 2012. Web. 16 Sep 2019.

Vancouver:

Oh SM. Modeling and Control of a Quad-Rotor Helicopter. [Internet] [Masters thesis]. University of Florida; 2012. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0044145.

Council of Science Editors:

Oh SM. Modeling and Control of a Quad-Rotor Helicopter. [Masters Thesis]. University of Florida; 2012. Available from: http://ufdc.ufl.edu/UFE0044145


University of Florida

3. Campos, Diego G. Effects of Isotropic Flexibility on Wings under a Plunging Motion.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2012, University of Florida

 In recent years there has been an interest in studying and understanding natural flyers to incorporate some of their features into small engineered flying systems.… (more)

Subjects/Keywords: Aerodynamics; Aircraft wings; Bending; Flexible wings; Kinematics; Lasers; Momentum; Stiffness; Velocity; Vorticity; bio-inspired  – flexibility  – fluid-structure  – interaction  – piv  – plunging

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APA (6th Edition):

Campos, D. G. (2012). Effects of Isotropic Flexibility on Wings under a Plunging Motion. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0044213

Chicago Manual of Style (16th Edition):

Campos, Diego G. “Effects of Isotropic Flexibility on Wings under a Plunging Motion.” 2012. Masters Thesis, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0044213.

MLA Handbook (7th Edition):

Campos, Diego G. “Effects of Isotropic Flexibility on Wings under a Plunging Motion.” 2012. Web. 16 Sep 2019.

Vancouver:

Campos DG. Effects of Isotropic Flexibility on Wings under a Plunging Motion. [Internet] [Masters thesis]. University of Florida; 2012. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0044213.

Council of Science Editors:

Campos DG. Effects of Isotropic Flexibility on Wings under a Plunging Motion. [Masters Thesis]. University of Florida; 2012. Available from: http://ufdc.ufl.edu/UFE0044213


University of Florida

4. Abudaram, Yaakov. Wind Tunnel Testing of Load-Alleviating Membrane Wings.

Degree: MS, Mechanical Engineering - Mechanical and Aerospace Engineering, 2009, University of Florida

 This work is concerned with wind tunnel testing of elastic latex and silicone membrane wings intended for micro air vehicles. Erratic flow conditions are a… (more)

Subjects/Keywords: Aircraft wings; Bending; Carbon fibers; Geometric angles; Images; Rigid wings; Silicones; Stall; Trailing edges; Wind tunnels; aerodynamic, aeroelastic, alleviating, anisotropic, attack, batten, camber, carbon, chord, deformation, drag, elongation, epoxy, fiber, hyperelastic, latex, leading, lift, mav, membrane, mold, pitching, reynolds, scallop, silicone, stall, sting, trailing, tunnel, vic, vortex, wind, wing

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APA (6th Edition):

Abudaram, Y. (2009). Wind Tunnel Testing of Load-Alleviating Membrane Wings. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0041340

Chicago Manual of Style (16th Edition):

Abudaram, Yaakov. “Wind Tunnel Testing of Load-Alleviating Membrane Wings.” 2009. Masters Thesis, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0041340.

MLA Handbook (7th Edition):

Abudaram, Yaakov. “Wind Tunnel Testing of Load-Alleviating Membrane Wings.” 2009. Web. 16 Sep 2019.

Vancouver:

Abudaram Y. Wind Tunnel Testing of Load-Alleviating Membrane Wings. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0041340.

Council of Science Editors:

Abudaram Y. Wind Tunnel Testing of Load-Alleviating Membrane Wings. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0041340


University of Florida

5. Love, Robert. Analysis of Aeroelastic Flapping-Wing Signals for Micro Air-Vehicles.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2009, University of Florida

 Flapping-wing micro air-vehicles are being investigated for their potential to provide enhanced aerodynamic efficiency, maneuverability and gust tolerance. The flight dynamics of flapping-wing micro air-vehicles… (more)

Subjects/Keywords: Aircraft wings; Amplitude; Dynamic structural analysis; Fourier transformations; Polynomials; Signals; Structural deflection; Trailing edges; Velocity; Wavelet analysis; aerial, aeroelastic, aeroservoelastic, aerospace, analysis, correlation, deflection, deformation, dic, digital, doppler, dynamics, engineer, flapping, fourier, ground, gvt, image, laser, ldv, mav, modal, mode, model, ornithopter, processing, signal, testing, uav, unmanned, vehicle, vibration, vibrometer, wavelet, wing

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APA (6th Edition):

Love, R. (2009). Analysis of Aeroelastic Flapping-Wing Signals for Micro Air-Vehicles. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0024479

Chicago Manual of Style (16th Edition):

Love, Robert. “Analysis of Aeroelastic Flapping-Wing Signals for Micro Air-Vehicles.” 2009. Masters Thesis, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0024479.

MLA Handbook (7th Edition):

Love, Robert. “Analysis of Aeroelastic Flapping-Wing Signals for Micro Air-Vehicles.” 2009. Web. 16 Sep 2019.

Vancouver:

Love R. Analysis of Aeroelastic Flapping-Wing Signals for Micro Air-Vehicles. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0024479.

Council of Science Editors:

Love R. Analysis of Aeroelastic Flapping-Wing Signals for Micro Air-Vehicles. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0024479


University of Florida

6. Lin, Albert. Fabrication and aeroelastic analysis of silicone membrane micro air vehicle wings.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2009, University of Florida

 Flexible wing micro air vehicles (MAVs) have been developed at the University of Florida to improve adverse flying conditions. Typically, such MAVs display low Reynolds… (more)

Subjects/Keywords: Aerodynamics; Aircraft wings; Bats; Carbon fibers; Design optimization; Latex; Silicone rubbers; Silicones; Topology; Vacuum; aeroelastic, deformation, fabrication, manufacturing, mav, membrane, silicone, uav, vic, wings

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APA (6th Edition):

Lin, A. (2009). Fabrication and aeroelastic analysis of silicone membrane micro air vehicle wings. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0041333

Chicago Manual of Style (16th Edition):

Lin, Albert. “Fabrication and aeroelastic analysis of silicone membrane micro air vehicle wings.” 2009. Masters Thesis, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0041333.

MLA Handbook (7th Edition):

Lin, Albert. “Fabrication and aeroelastic analysis of silicone membrane micro air vehicle wings.” 2009. Web. 16 Sep 2019.

Vancouver:

Lin A. Fabrication and aeroelastic analysis of silicone membrane micro air vehicle wings. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0041333.

Council of Science Editors:

Lin A. Fabrication and aeroelastic analysis of silicone membrane micro air vehicle wings. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0041333


University of Florida

7. Johnson, Baron. High Angle-of-Attack Flight Characteristics of a Small UAV with a Variable-Size Vertical Tail.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2009, University of Florida

 The angle-of-attack parameter has a significant influence on the aerodynamics, flight dynamics, and handling qualities of aircraft. Flight at high angle-of-attack conditions enables many missions;… (more)

Subjects/Keywords: Ailerons; Aircraft; Aircraft pitch; Aircraft roll; Flight stabilizers; Signals; Structural deflection; Vehicular flight; Wavelet analysis; Wing rock; 3d, aircraft, alpha, angle, attack, baron, harrier, high, inverted, lind, mav, of, rc, rock, showtime, tail, uav, upright, vertical, wing

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APA (6th Edition):

Johnson, B. (2009). High Angle-of-Attack Flight Characteristics of a Small UAV with a Variable-Size Vertical Tail. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0024449

Chicago Manual of Style (16th Edition):

Johnson, Baron. “High Angle-of-Attack Flight Characteristics of a Small UAV with a Variable-Size Vertical Tail.” 2009. Masters Thesis, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0024449.

MLA Handbook (7th Edition):

Johnson, Baron. “High Angle-of-Attack Flight Characteristics of a Small UAV with a Variable-Size Vertical Tail.” 2009. Web. 16 Sep 2019.

Vancouver:

Johnson B. High Angle-of-Attack Flight Characteristics of a Small UAV with a Variable-Size Vertical Tail. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0024449.

Council of Science Editors:

Johnson B. High Angle-of-Attack Flight Characteristics of a Small UAV with a Variable-Size Vertical Tail. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0024449


University of Florida

8. Hurley, Ryan. Three-Dimensional Trajectory Generation for Flight Within an Obstacle Rich Environment.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2009, University of Florida

 Autonomous flight through urban environments requires methods to generate trajectories that traverse the region and its associated obstacles. This thesis introduces the development of a… (more)

Subjects/Keywords: Aircraft maneuvers; City planning; Kinetics; Robotics; Simulations; Trajectories; Travel time; Tree growth; Vehicles; Walkways; aerial, air, airplane, autonomous, avoidance, bridge, building, city, dense, dimension, dimensional, dubins, hurley, lind, mav, micro, obstacle, path, planning, random, ryan, structure, three, trajectory, tree, two, uav, unmanned, urban, vehicle

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APA (6th Edition):

Hurley, R. (2009). Three-Dimensional Trajectory Generation for Flight Within an Obstacle Rich Environment. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0024478

Chicago Manual of Style (16th Edition):

Hurley, Ryan. “Three-Dimensional Trajectory Generation for Flight Within an Obstacle Rich Environment.” 2009. Masters Thesis, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0024478.

MLA Handbook (7th Edition):

Hurley, Ryan. “Three-Dimensional Trajectory Generation for Flight Within an Obstacle Rich Environment.” 2009. Web. 16 Sep 2019.

Vancouver:

Hurley R. Three-Dimensional Trajectory Generation for Flight Within an Obstacle Rich Environment. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0024478.

Council of Science Editors:

Hurley R. Three-Dimensional Trajectory Generation for Flight Within an Obstacle Rich Environment. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0024478


University of Florida

9. Roberts, Brian. Turn Performance and Flight Dynamics of a Pterosaur and a Pterosaur-Inspired Variable-Placement Vertical Tail Aircraft.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2009, University of Florida

 Mission performance for small aircraft is often dependent on turn radius. Various biologically-inspired concepts have demonstrated that performance can be improved by morphing the wings… (more)

Subjects/Keywords: Ailerons; Aircraft; Aircraft roll; Aircraft wings; Center of mass; Elbow joint; Elevators; Flight stabilizers; Sideslip; Structural deflection; dynamics, flight, mav, performance, pterosaur, radius, tail, turn, uav, vertical

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APA (6th Edition):

Roberts, B. (2009). Turn Performance and Flight Dynamics of a Pterosaur and a Pterosaur-Inspired Variable-Placement Vertical Tail Aircraft. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0024421

Chicago Manual of Style (16th Edition):

Roberts, Brian. “Turn Performance and Flight Dynamics of a Pterosaur and a Pterosaur-Inspired Variable-Placement Vertical Tail Aircraft.” 2009. Masters Thesis, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0024421.

MLA Handbook (7th Edition):

Roberts, Brian. “Turn Performance and Flight Dynamics of a Pterosaur and a Pterosaur-Inspired Variable-Placement Vertical Tail Aircraft.” 2009. Web. 16 Sep 2019.

Vancouver:

Roberts B. Turn Performance and Flight Dynamics of a Pterosaur and a Pterosaur-Inspired Variable-Placement Vertical Tail Aircraft. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0024421.

Council of Science Editors:

Roberts B. Turn Performance and Flight Dynamics of a Pterosaur and a Pterosaur-Inspired Variable-Placement Vertical Tail Aircraft. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0024421


University of Florida

10. Kumar, Preethi. Path-Planning with Temporal Constraints for Sensing Missions with Agile Vehicles.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2012, University of Florida

 The miniaturization of control systems technology has led to a class of highly agile, easily maneuverable Unmanned Aerial Vehicles that can be used for search… (more)

Subjects/Keywords: Connectivity; Detection; Distance functions; Field of view; Kinetics; Remotely piloted vehicles; Sensors; Simulations; Trajectories; Velocity; constraint  – path  – planning  – sensing  – temporal  – uav

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APA (6th Edition):

Kumar, P. (2012). Path-Planning with Temporal Constraints for Sensing Missions with Agile Vehicles. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0044296

Chicago Manual of Style (16th Edition):

Kumar, Preethi. “Path-Planning with Temporal Constraints for Sensing Missions with Agile Vehicles.” 2012. Masters Thesis, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0044296.

MLA Handbook (7th Edition):

Kumar, Preethi. “Path-Planning with Temporal Constraints for Sensing Missions with Agile Vehicles.” 2012. Web. 16 Sep 2019.

Vancouver:

Kumar P. Path-Planning with Temporal Constraints for Sensing Missions with Agile Vehicles. [Internet] [Masters thesis]. University of Florida; 2012. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0044296.

Council of Science Editors:

Kumar P. Path-Planning with Temporal Constraints for Sensing Missions with Agile Vehicles. [Masters Thesis]. University of Florida; 2012. Available from: http://ufdc.ufl.edu/UFE0044296


University of Florida

11. Sallstrom,Erik M. Flow field of flexible flapping wings.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2011, University of Florida

 The agility and maneuverability of natural fliers would be desirable to incorporate into engineered micro air vehicles (MAVs). However, there is still much for engineers… (more)

Subjects/Keywords: Aircraft wings; Flow distribution; Hovering; Lasers; Leading edges; Photographs; Pixels; Seeding; Velocity; Vorticity; aerodynamics  – dynamics  – flapping  – flexible  – flight  – fluid  – image  – interaction  – particle  – piv  – structure  – unsteady  – velocimetry  – wings

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APA (6th Edition):

M, S. (2011). Flow field of flexible flapping wings. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0042772

Chicago Manual of Style (16th Edition):

M, Sallstrom,Erik. “Flow field of flexible flapping wings.” 2011. Doctoral Dissertation, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0042772.

MLA Handbook (7th Edition):

M, Sallstrom,Erik. “Flow field of flexible flapping wings.” 2011. Web. 16 Sep 2019.

Vancouver:

M S. Flow field of flexible flapping wings. [Internet] [Doctoral dissertation]. University of Florida; 2011. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0042772.

Council of Science Editors:

M S. Flow field of flexible flapping wings. [Doctoral Dissertation]. University of Florida; 2011. Available from: http://ufdc.ufl.edu/UFE0042772


University of Florida

12. Cobb, James T. Sonar Image Modeling for Texture Discrimination and Classification.

Degree: PhD, Electrical and Computer Engineering, 2011, University of Florida

 High-resolution synthetic aperture sonar (SAS) systems yield finely detailedimages of sea bed environments. SAS image texture models must be capable ofrepresenting a wide variety of… (more)

Subjects/Keywords: Imaging; Mathematical independent variables; Ocean floor; Parametric models; Pixels; Rock textures; Sand ripples; Sonar; Statistical models; Statistics; autocorrelation  – expectation-maximization  – k-distribution  – segmentation  – sonar

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APA (6th Edition):

Cobb, J. T. (2011). Sonar Image Modeling for Texture Discrimination and Classification. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0043611

Chicago Manual of Style (16th Edition):

Cobb, James T. “Sonar Image Modeling for Texture Discrimination and Classification.” 2011. Doctoral Dissertation, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0043611.

MLA Handbook (7th Edition):

Cobb, James T. “Sonar Image Modeling for Texture Discrimination and Classification.” 2011. Web. 16 Sep 2019.

Vancouver:

Cobb JT. Sonar Image Modeling for Texture Discrimination and Classification. [Internet] [Doctoral dissertation]. University of Florida; 2011. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0043611.

Council of Science Editors:

Cobb JT. Sonar Image Modeling for Texture Discrimination and Classification. [Doctoral Dissertation]. University of Florida; 2011. Available from: http://ufdc.ufl.edu/UFE0043611


University of Florida

13. GRANT,DANIEL THURMOND. A Linear Input-Varying Framework for Modeling and Control of Morphing Aircraft.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2011, University of Florida

 Morphing, which changes the shape and configuration of an aircraft, is being adopted to expand mission capabilities of aircraft. The introduction of biological-inspired morphing is… (more)

Subjects/Keywords: Aircraft; Aircraft maneuvers; Aircraft wings; Damping; Eigenvectors; Inertia; Polynomials; Sine function; Trajectories; Velocity; AIRCRAFT  – CONTROL  – DYNAMICS  – MORPHING  – UNMANNED

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APA (6th Edition):

THURMOND, G. (2011). A Linear Input-Varying Framework for Modeling and Control of Morphing Aircraft. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0042424

Chicago Manual of Style (16th Edition):

THURMOND, GRANT,DANIEL. “A Linear Input-Varying Framework for Modeling and Control of Morphing Aircraft.” 2011. Doctoral Dissertation, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0042424.

MLA Handbook (7th Edition):

THURMOND, GRANT,DANIEL. “A Linear Input-Varying Framework for Modeling and Control of Morphing Aircraft.” 2011. Web. 16 Sep 2019.

Vancouver:

THURMOND G. A Linear Input-Varying Framework for Modeling and Control of Morphing Aircraft. [Internet] [Doctoral dissertation]. University of Florida; 2011. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0042424.

Council of Science Editors:

THURMOND G. A Linear Input-Varying Framework for Modeling and Control of Morphing Aircraft. [Doctoral Dissertation]. University of Florida; 2011. Available from: http://ufdc.ufl.edu/UFE0042424


University of Florida

14. Love,Robert D. An Experimentally-Based Procedure for Aeroservoelastic Model Identification and Control Synthesis for Morphing and Flapping Wings.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2011, University of Florida

 Morphing and flapping wings are enabling technologies for vehicles of the future. Vehicles with morphing and flapping wings will have greater mission capability and flexibility… (more)

Subjects/Keywords: Aerodynamics; Aircraft; Aircraft wings; Dynamic structural analysis; Kinematics; Modeling; Piezoelectric actuators; Sensors; Signals; Structural deflection; aeroelastic  – aeroelasticity  – aeroservoelastic  – aeroservoelasticity  – aerospace  – aircraft  – analysis  – basis  – control  – design  – dynamics  – experimental  – feedback  – feedforward  – flapping  – flexibility  – flexible  – flight  – frequency  – hydroelasticity  – identification  – interdisciplinary  – mav  – mechanics  – model  – morphing  – optimization  – performance  – periodic  – processing  – robustness  – sensor  – shape  – signal  – structural  – time  – uav  – wing  – wings

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APA (6th Edition):

D, L. (2011). An Experimentally-Based Procedure for Aeroservoelastic Model Identification and Control Synthesis for Morphing and Flapping Wings. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0043309

Chicago Manual of Style (16th Edition):

D, Love,Robert. “An Experimentally-Based Procedure for Aeroservoelastic Model Identification and Control Synthesis for Morphing and Flapping Wings.” 2011. Doctoral Dissertation, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0043309.

MLA Handbook (7th Edition):

D, Love,Robert. “An Experimentally-Based Procedure for Aeroservoelastic Model Identification and Control Synthesis for Morphing and Flapping Wings.” 2011. Web. 16 Sep 2019.

Vancouver:

D L. An Experimentally-Based Procedure for Aeroservoelastic Model Identification and Control Synthesis for Morphing and Flapping Wings. [Internet] [Doctoral dissertation]. University of Florida; 2011. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0043309.

Council of Science Editors:

D L. An Experimentally-Based Procedure for Aeroservoelastic Model Identification and Control Synthesis for Morphing and Flapping Wings. [Doctoral Dissertation]. University of Florida; 2011. Available from: http://ufdc.ufl.edu/UFE0043309


University of Florida

15. Wilcox, Zachary. Nonlinear Control of Linear Parameter Varying Systems with Applications to Hypersonic Vehicles.

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

 The focus of this dissertation is to design a controller for linear parameter varying (LPV) systems, apply it specifically to air-breathing hypersonic vehicles, and examine… (more)

Subjects/Keywords: Cost functions; Design analysis; Dynamic modeling; Hypersonic aircraft; Matrices; Modeling; Parametric models; Simulations; Temperature profiles; Velocity; aerospace, aircraft, controls, hypersonic, linear, lpv, nonlinear, parameter, robust, varying, vehicle

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APA (6th Edition):

Wilcox, Z. (2010). Nonlinear Control of Linear Parameter Varying Systems with Applications to Hypersonic Vehicles. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0041960

Chicago Manual of Style (16th Edition):

Wilcox, Zachary. “Nonlinear Control of Linear Parameter Varying Systems with Applications to Hypersonic Vehicles.” 2010. Doctoral Dissertation, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0041960.

MLA Handbook (7th Edition):

Wilcox, Zachary. “Nonlinear Control of Linear Parameter Varying Systems with Applications to Hypersonic Vehicles.” 2010. Web. 16 Sep 2019.

Vancouver:

Wilcox Z. Nonlinear Control of Linear Parameter Varying Systems with Applications to Hypersonic Vehicles. [Internet] [Doctoral dissertation]. University of Florida; 2010. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0041960.

Council of Science Editors:

Wilcox Z. Nonlinear Control of Linear Parameter Varying Systems with Applications to Hypersonic Vehicles. [Doctoral Dissertation]. University of Florida; 2010. Available from: http://ufdc.ufl.edu/UFE0041960


University of Florida

16. Roberts, Brian C. Polynomial Chaos Analysis of Micro Air Vehicles in Turbulence.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2012, University of Florida

 Use of unmanned vehicles is expected to continue to grow. As the variety of missions conducted by unmanned vehicles increases, these vehicles will require greater… (more)

Subjects/Keywords: Aircraft; Aircraft wings; Chaos; Eigenvalues; Modeling; Polynomials; Sine function; Turbulence; Turbulence models; Wind tunnels; chaos  – microairvehicle  – path  – polynomial  – turbulence  – uncertainty

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APA (6th Edition):

Roberts, B. C. (2012). Polynomial Chaos Analysis of Micro Air Vehicles in Turbulence. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0043683

Chicago Manual of Style (16th Edition):

Roberts, Brian C. “Polynomial Chaos Analysis of Micro Air Vehicles in Turbulence.” 2012. Doctoral Dissertation, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0043683.

MLA Handbook (7th Edition):

Roberts, Brian C. “Polynomial Chaos Analysis of Micro Air Vehicles in Turbulence.” 2012. Web. 16 Sep 2019.

Vancouver:

Roberts BC. Polynomial Chaos Analysis of Micro Air Vehicles in Turbulence. [Internet] [Doctoral dissertation]. University of Florida; 2012. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0043683.

Council of Science Editors:

Roberts BC. Polynomial Chaos Analysis of Micro Air Vehicles in Turbulence. [Doctoral Dissertation]. University of Florida; 2012. Available from: http://ufdc.ufl.edu/UFE0043683


University of Florida

17. Grant, Daniel. Modeling and Dynamic Analysis of a Multi-Joint Morphing Aircraft.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2009, University of Florida

 Morphing, which changes the shape and configuration of an aircraft, is being adopted to expand mission capabilities of aircraft. The introduction of biological-inspired morphing is… (more)

Subjects/Keywords: Aerodynamics; Aircraft; Aircraft maneuvers; Aircraft pitch; Aircraft roll; Aircraft wings; Altitude; Coordinate systems; Inertia; Sine function; daniel, grant, lind, morphing, uav

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APA (6th Edition):

Grant, D. (2009). Modeling and Dynamic Analysis of a Multi-Joint Morphing Aircraft. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0024477

Chicago Manual of Style (16th Edition):

Grant, Daniel. “Modeling and Dynamic Analysis of a Multi-Joint Morphing Aircraft.” 2009. Masters Thesis, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0024477.

MLA Handbook (7th Edition):

Grant, Daniel. “Modeling and Dynamic Analysis of a Multi-Joint Morphing Aircraft.” 2009. Web. 16 Sep 2019.

Vancouver:

Grant D. Modeling and Dynamic Analysis of a Multi-Joint Morphing Aircraft. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0024477.

Council of Science Editors:

Grant D. Modeling and Dynamic Analysis of a Multi-Joint Morphing Aircraft. [Masters Thesis]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0024477


University of Florida

18. Pasiliao, Crystal. Temporal Analysis of Transonic Flow Field Characteristics Associated with Limit Cycle Oscillations.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2009, University of Florida

 Limit Cycle Oscillation (LCO) is a sustained, non-divergent, periodic motion experienced by aircraft with certain external store configurations. Flutter, an instability caused by the aerodynamic… (more)

Subjects/Keywords: Aerodynamics; Aircraft; Aircraft pitch; Aircraft roll; Aircraft wings; Charge flow devices; Fast Fourier transformations; Limit cycles; Oscillation; Transonic flow

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APA (6th Edition):

Pasiliao, C. (2009). Temporal Analysis of Transonic Flow Field Characteristics Associated with Limit Cycle Oscillations. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0024231

Chicago Manual of Style (16th Edition):

Pasiliao, Crystal. “Temporal Analysis of Transonic Flow Field Characteristics Associated with Limit Cycle Oscillations.” 2009. Doctoral Dissertation, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0024231.

MLA Handbook (7th Edition):

Pasiliao, Crystal. “Temporal Analysis of Transonic Flow Field Characteristics Associated with Limit Cycle Oscillations.” 2009. Web. 16 Sep 2019.

Vancouver:

Pasiliao C. Temporal Analysis of Transonic Flow Field Characteristics Associated with Limit Cycle Oscillations. [Internet] [Doctoral dissertation]. University of Florida; 2009. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0024231.

Council of Science Editors:

Pasiliao C. Temporal Analysis of Transonic Flow Field Characteristics Associated with Limit Cycle Oscillations. [Doctoral Dissertation]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0024231


University of Florida

19. Hao, He. Distributed Control of Multi-agent Systems Performance Scaling with Network Size.

Degree: PhD, Mechanical Engineering - Mechanical and Aerospace Engineering, 2012, University of Florida

 The goal of distributed control of multi-agent systems (MASs) is to achieve a global control objective while using only locally available information. Each agent computes… (more)

Subjects/Keywords: Approximation; Asymmetry; Boundary conditions; Conceptual lattices; Eigenvalues; Mathematical robustness; Modeling; Power laws; Trajectories; Velocity; asymmetricdesign  – convergencerate  – distributedcontrol  – multiagentsystems  – performancescaling  – robustness

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APA (6th Edition):

Hao, H. (2012). Distributed Control of Multi-agent Systems Performance Scaling with Network Size. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0044859

Chicago Manual of Style (16th Edition):

Hao, He. “Distributed Control of Multi-agent Systems Performance Scaling with Network Size.” 2012. Doctoral Dissertation, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0044859.

MLA Handbook (7th Edition):

Hao, He. “Distributed Control of Multi-agent Systems Performance Scaling with Network Size.” 2012. Web. 16 Sep 2019.

Vancouver:

Hao H. Distributed Control of Multi-agent Systems Performance Scaling with Network Size. [Internet] [Doctoral dissertation]. University of Florida; 2012. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0044859.

Council of Science Editors:

Hao H. Distributed Control of Multi-agent Systems Performance Scaling with Network Size. [Doctoral Dissertation]. University of Florida; 2012. Available from: http://ufdc.ufl.edu/UFE0044859


University of Florida

20. Carter, Ryan Elliot. System Identification and Trajectory Optimization for Guided Store Separation.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2012, University of Florida

 Combat aircraft utilize expendable stores such as missiles, bombs, flares, and external tanks to execute their missions.  Safe and acceptable separation of these stores from… (more)

Subjects/Keywords: Aerodynamics; Aircraft; Flight conditions; Flight tests; Parametric models; Simulations; Sine function; System identification; Trajectories; Velocity; autopilot  – control  – identification  – neighboring  – optimal  – optimization  – separation  – store  – system  – trajectory

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APA (6th Edition):

Carter, R. E. (2012). System Identification and Trajectory Optimization for Guided Store Separation. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0044483

Chicago Manual of Style (16th Edition):

Carter, Ryan Elliot. “System Identification and Trajectory Optimization for Guided Store Separation.” 2012. Doctoral Dissertation, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0044483.

MLA Handbook (7th Edition):

Carter, Ryan Elliot. “System Identification and Trajectory Optimization for Guided Store Separation.” 2012. Web. 16 Sep 2019.

Vancouver:

Carter RE. System Identification and Trajectory Optimization for Guided Store Separation. [Internet] [Doctoral dissertation]. University of Florida; 2012. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0044483.

Council of Science Editors:

Carter RE. System Identification and Trajectory Optimization for Guided Store Separation. [Doctoral Dissertation]. University of Florida; 2012. Available from: http://ufdc.ufl.edu/UFE0044483


University of Florida

21. Bhat, Sanketh. Control-Oriented Design of Systems with Operating Ranges to Optimize Closed-Loop Performance.

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

 Traditionally, the design of structural systems and vehicles has focused first on the design of the structure and then the control and other aspects are… (more)

Subjects/Keywords: Design analysis; Design optimization; Distance functions; Elevators; Hypersonic aircraft; Kriging; Mathematical variables; Systems design; Vibration; Weighting functions; control, hypersonic, linear, surrogate

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APA (6th Edition):

Bhat, S. (2010). Control-Oriented Design of Systems with Operating Ranges to Optimize Closed-Loop Performance. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0042357

Chicago Manual of Style (16th Edition):

Bhat, Sanketh. “Control-Oriented Design of Systems with Operating Ranges to Optimize Closed-Loop Performance.” 2010. Doctoral Dissertation, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0042357.

MLA Handbook (7th Edition):

Bhat, Sanketh. “Control-Oriented Design of Systems with Operating Ranges to Optimize Closed-Loop Performance.” 2010. Web. 16 Sep 2019.

Vancouver:

Bhat S. Control-Oriented Design of Systems with Operating Ranges to Optimize Closed-Loop Performance. [Internet] [Doctoral dissertation]. University of Florida; 2010. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0042357.

Council of Science Editors:

Bhat S. Control-Oriented Design of Systems with Operating Ranges to Optimize Closed-Loop Performance. [Doctoral Dissertation]. University of Florida; 2010. Available from: http://ufdc.ufl.edu/UFE0042357


University of Florida

22. Mehta, Siddhartha. A Daisy-Chaining Approach for Vision-Based Control and Estimation.

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

 A DAISY-CHAINING APPROACH FOR VISION-BASED CONTROL AND ESTIMATION The research presented in this dissertation monograph lies within the general scope of guidance, navigation, and control… (more)

Subjects/Keywords: Coordinate systems; Estimation methods; Homography; Image rotation; Monoculars; Moving images; Outliers; Robots; Servomotors; Trajectories; collaborative, control, cooperative, daisy, nonlinear, pegus, ransac, robust, slam, uav, ugv, vision, visual

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APA (6th Edition):

Mehta, S. (2010). A Daisy-Chaining Approach for Vision-Based Control and Estimation. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0041119

Chicago Manual of Style (16th Edition):

Mehta, Siddhartha. “A Daisy-Chaining Approach for Vision-Based Control and Estimation.” 2010. Doctoral Dissertation, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0041119.

MLA Handbook (7th Edition):

Mehta, Siddhartha. “A Daisy-Chaining Approach for Vision-Based Control and Estimation.” 2010. Web. 16 Sep 2019.

Vancouver:

Mehta S. A Daisy-Chaining Approach for Vision-Based Control and Estimation. [Internet] [Doctoral dissertation]. University of Florida; 2010. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0041119.

Council of Science Editors:

Mehta S. A Daisy-Chaining Approach for Vision-Based Control and Estimation. [Doctoral Dissertation]. University of Florida; 2010. Available from: http://ufdc.ufl.edu/UFE0041119


University of Florida

23. Patre, Parag. Lyapunov-Based Robust and Adaptive Control of Nonlinear Systems Using a Novel Feedback Structure.

Degree: PhD, Mechanical Engineering - Mechanical and Aerospace Engineering, 2009, University of Florida

 The focus of this research is an examination of the interplay between different intelligent feedforward mechanisms with a recently developed continuous robust feedback mechanism, coined… (more)

Subjects/Keywords: Adaptive control; Error rates; Feedback control; Governing laws clause; Human error; Matrices; Neural networks; Sufficient conditions; Torque; Trajectories; adaptive, composite, control, disturbances, networks, neural, nonlinear, rise, robust, uncertain

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APA (6th Edition):

Patre, P. (2009). Lyapunov-Based Robust and Adaptive Control of Nonlinear Systems Using a Novel Feedback Structure. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0024807

Chicago Manual of Style (16th Edition):

Patre, Parag. “Lyapunov-Based Robust and Adaptive Control of Nonlinear Systems Using a Novel Feedback Structure.” 2009. Doctoral Dissertation, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0024807.

MLA Handbook (7th Edition):

Patre, Parag. “Lyapunov-Based Robust and Adaptive Control of Nonlinear Systems Using a Novel Feedback Structure.” 2009. Web. 16 Sep 2019.

Vancouver:

Patre P. Lyapunov-Based Robust and Adaptive Control of Nonlinear Systems Using a Novel Feedback Structure. [Internet] [Doctoral dissertation]. University of Florida; 2009. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0024807.

Council of Science Editors:

Patre P. Lyapunov-Based Robust and Adaptive Control of Nonlinear Systems Using a Novel Feedback Structure. [Doctoral Dissertation]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0024807


University of Florida

24. Khambatta, Parvez. Aerodynamic Characterization of Flow over a Three-Dimensional Rigid Micro Air Vehicle Wing.

Degree: MS, Mechanical Engineering - Mechanical and Aerospace Engineering, 2008, University of Florida

 With an increase in the study and development of Micro Air Vehicles in recent years, the research in this document hopes to shed some light… (more)

Subjects/Keywords: Aerodynamics; Aircraft wings; Airfoils; Cross correlation; Low reynolds number; Pixels; Shear layers; Turbulence; Velocity; Vorticity; aerodynamic, air, calibration, characteristics, characterization, flow, hot, image, low, mav, micro, number, particle, piv, reynolds, rigid, vehicle, velocimetry, wing, wire

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APA (6th Edition):

Khambatta, P. (2008). Aerodynamic Characterization of Flow over a Three-Dimensional Rigid Micro Air Vehicle Wing. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0022718

Chicago Manual of Style (16th Edition):

Khambatta, Parvez. “Aerodynamic Characterization of Flow over a Three-Dimensional Rigid Micro Air Vehicle Wing.” 2008. Masters Thesis, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0022718.

MLA Handbook (7th Edition):

Khambatta, Parvez. “Aerodynamic Characterization of Flow over a Three-Dimensional Rigid Micro Air Vehicle Wing.” 2008. Web. 16 Sep 2019.

Vancouver:

Khambatta P. Aerodynamic Characterization of Flow over a Three-Dimensional Rigid Micro Air Vehicle Wing. [Internet] [Masters thesis]. University of Florida; 2008. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0022718.

Council of Science Editors:

Khambatta P. Aerodynamic Characterization of Flow over a Three-Dimensional Rigid Micro Air Vehicle Wing. [Masters Thesis]. University of Florida; 2008. Available from: http://ufdc.ufl.edu/UFE0022718


University of Florida

25. Regisford, Sean James Sidney, 1977-. Topics in the Structural Dynamics and Control of an Articulated Micro Air Vehicle.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2008, University of Florida

 This work presents a methodology to determine of accurate computer models of articulated micro air vehicles. Prior to this work, much of the innovation in… (more)

Subjects/Keywords: Aircraft; Aircraft wings; Coordinate systems; Equations of motion; Fuselages; Kinetic energy; Matrices; Modeling; Optimal control; Simulations

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APA (6th Edition):

Regisford, Sean James Sidney, 1. (2008). Topics in the Structural Dynamics and Control of an Articulated Micro Air Vehicle. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0021668

Chicago Manual of Style (16th Edition):

Regisford, Sean James Sidney, 1977-. “Topics in the Structural Dynamics and Control of an Articulated Micro Air Vehicle.” 2008. Doctoral Dissertation, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0021668.

MLA Handbook (7th Edition):

Regisford, Sean James Sidney, 1977-. “Topics in the Structural Dynamics and Control of an Articulated Micro Air Vehicle.” 2008. Web. 16 Sep 2019.

Vancouver:

Regisford, Sean James Sidney 1. Topics in the Structural Dynamics and Control of an Articulated Micro Air Vehicle. [Internet] [Doctoral dissertation]. University of Florida; 2008. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0021668.

Council of Science Editors:

Regisford, Sean James Sidney 1. Topics in the Structural Dynamics and Control of an Articulated Micro Air Vehicle. [Doctoral Dissertation]. University of Florida; 2008. Available from: http://ufdc.ufl.edu/UFE0021668


University of Florida

26. Branch, Eric Alan. Multi-Vehicle Cooperative Control for Vision-Based Environment Mapping.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2007, University of Florida

 Flight within urban environments is currently achievable using small and agile aircraft; however, the path planning for such vehicles is difficult due to the unknown… (more)

Subjects/Keywords: Aircraft; Datasets; Genetic mapping; Geometric planes; Mapping; Mathematical vectors; Robots; Sensors; Simulations; Trajectories; cooperative, mapping, mav, planning, vision

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APA (6th Edition):

Branch, E. A. (2007). Multi-Vehicle Cooperative Control for Vision-Based Environment Mapping. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0019741

Chicago Manual of Style (16th Edition):

Branch, Eric Alan. “Multi-Vehicle Cooperative Control for Vision-Based Environment Mapping.” 2007. Masters Thesis, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0019741.

MLA Handbook (7th Edition):

Branch, Eric Alan. “Multi-Vehicle Cooperative Control for Vision-Based Environment Mapping.” 2007. Web. 16 Sep 2019.

Vancouver:

Branch EA. Multi-Vehicle Cooperative Control for Vision-Based Environment Mapping. [Internet] [Masters thesis]. University of Florida; 2007. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0019741.

Council of Science Editors:

Branch EA. Multi-Vehicle Cooperative Control for Vision-Based Environment Mapping. [Masters Thesis]. University of Florida; 2007. Available from: http://ufdc.ufl.edu/UFE0019741


University of Florida

27. Bhat, Sanketh. Control-Oriented Analysis of Aerothermoelastic Effects for a Hypersonic Vehicle.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2008, University of Florida

 Hypersonic flight is seen as a feasible solution to make space travel faster, safer and more affordable. The design of the Air-breathing hypersonic vehicle is… (more)

Subjects/Keywords: Damping; Design analysis; Design optimization; Dynamic structural analysis; Fuselages; Hypersonic aircraft; Hypersonics; Modeling; Temperature profiles; Vibration; aerothermoelasticity, control, hypersonic, parameter, varying

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APA (6th Edition):

Bhat, S. (2008). Control-Oriented Analysis of Aerothermoelastic Effects for a Hypersonic Vehicle. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0024107

Chicago Manual of Style (16th Edition):

Bhat, Sanketh. “Control-Oriented Analysis of Aerothermoelastic Effects for a Hypersonic Vehicle.” 2008. Masters Thesis, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0024107.

MLA Handbook (7th Edition):

Bhat, Sanketh. “Control-Oriented Analysis of Aerothermoelastic Effects for a Hypersonic Vehicle.” 2008. Web. 16 Sep 2019.

Vancouver:

Bhat S. Control-Oriented Analysis of Aerothermoelastic Effects for a Hypersonic Vehicle. [Internet] [Masters thesis]. University of Florida; 2008. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0024107.

Council of Science Editors:

Bhat S. Control-Oriented Analysis of Aerothermoelastic Effects for a Hypersonic Vehicle. [Masters Thesis]. University of Florida; 2008. Available from: http://ufdc.ufl.edu/UFE0024107


University of Florida

28. Watkins, Adam Scott. Vision-Based Map Building and Trajectory Planning to Enable Autonomous Flight through Urban Environments.

Degree: PhD, Mechanical Engineering - Mechanical and Aerospace Engineering, 2007, University of Florida

 The desire to use unmanned air vehicles (UAVs) in a variety of complex missions has motivated the need to increase the autonomous capabilities of these… (more)

Subjects/Keywords: Aircraft; Algorithms; Covariance; Genetic mapping; Landmarks; Navigation; Robotics; Sensors; State estimation; Trajectories; autonomous, map, particle, slam, trajectory, unmanned

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APA (6th Edition):

Watkins, A. S. (2007). Vision-Based Map Building and Trajectory Planning to Enable Autonomous Flight through Urban Environments. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0021230

Chicago Manual of Style (16th Edition):

Watkins, Adam Scott. “Vision-Based Map Building and Trajectory Planning to Enable Autonomous Flight through Urban Environments.” 2007. Doctoral Dissertation, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0021230.

MLA Handbook (7th Edition):

Watkins, Adam Scott. “Vision-Based Map Building and Trajectory Planning to Enable Autonomous Flight through Urban Environments.” 2007. Web. 16 Sep 2019.

Vancouver:

Watkins AS. Vision-Based Map Building and Trajectory Planning to Enable Autonomous Flight through Urban Environments. [Internet] [Doctoral dissertation]. University of Florida; 2007. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0021230.

Council of Science Editors:

Watkins AS. Vision-Based Map Building and Trajectory Planning to Enable Autonomous Flight through Urban Environments. [Doctoral Dissertation]. University of Florida; 2007. Available from: http://ufdc.ufl.edu/UFE0021230


University of Florida

29. Abdul-Rahim, Mujahid. Maneuvering Control and Configuration Adaptation of a Biologically Inspired Morphing Aircraft.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2007, University of Florida

 Natural flight as a source of inspiration for aircraft design was prominent with early aircraft but became marginalized as aircraft became larger and faster. With… (more)

Subjects/Keywords: Aircraft; Aircraft maneuvers; Aircraft roll; Aircraft wings; Animal wings; Birds; Distance functions; Geometric shapes; Trajectories; Vehicular flight; adaptation, adaptive, alfred, avian, biological, bird, chicken, configuration, control, flight, inspiration, maneuvering, metric, model, morphing, optimal, reference, rubber, trajectory

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APA (6th Edition):

Abdul-Rahim, M. (2007). Maneuvering Control and Configuration Adaptation of a Biologically Inspired Morphing Aircraft. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0016721

Chicago Manual of Style (16th Edition):

Abdul-Rahim, Mujahid. “Maneuvering Control and Configuration Adaptation of a Biologically Inspired Morphing Aircraft.” 2007. Doctoral Dissertation, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0016721.

MLA Handbook (7th Edition):

Abdul-Rahim, Mujahid. “Maneuvering Control and Configuration Adaptation of a Biologically Inspired Morphing Aircraft.” 2007. Web. 16 Sep 2019.

Vancouver:

Abdul-Rahim M. Maneuvering Control and Configuration Adaptation of a Biologically Inspired Morphing Aircraft. [Internet] [Doctoral dissertation]. University of Florida; 2007. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0016721.

Council of Science Editors:

Abdul-Rahim M. Maneuvering Control and Configuration Adaptation of a Biologically Inspired Morphing Aircraft. [Doctoral Dissertation]. University of Florida; 2007. Available from: http://ufdc.ufl.edu/UFE0016721


University of Florida

30. JOHNSON,BARON. Trajectory Planning for Effective Close-Proximity Sensing with Agile Vehicles.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2011, University of Florida

Unmanned systems are expected to continue growing in usefulness for surveillance Advisors/Committee Members: Lind, Richard C (committee chair), Barooah, Prabir (committee member), Ifju, Peter (committee member), Burks, Thomas F (committee member).

Subjects/Keywords: Aircraft; Aircraft roll; Cost functions; Detection; Distance functions; Monte Carlo methods; Sensors; Trajectories; Velocity; Wing rock; ALPHA  – PATH  – PLANNING  – RDT  – RRT  – SENSING  – SENSOR  – SURROGATE  – TRAJECTORY  – UAS  – UAV  – UNMANNED

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APA (6th Edition):

JOHNSON,BARON. (2011). Trajectory Planning for Effective Close-Proximity Sensing with Agile Vehicles. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0042697

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Chicago Manual of Style (16th Edition):

JOHNSON,BARON. “Trajectory Planning for Effective Close-Proximity Sensing with Agile Vehicles.” 2011. Doctoral Dissertation, University of Florida. Accessed September 16, 2019. http://ufdc.ufl.edu/UFE0042697.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

MLA Handbook (7th Edition):

JOHNSON,BARON. “Trajectory Planning for Effective Close-Proximity Sensing with Agile Vehicles.” 2011. Web. 16 Sep 2019.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

JOHNSON,BARON. Trajectory Planning for Effective Close-Proximity Sensing with Agile Vehicles. [Internet] [Doctoral dissertation]. University of Florida; 2011. [cited 2019 Sep 16]. Available from: http://ufdc.ufl.edu/UFE0042697.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Council of Science Editors:

JOHNSON,BARON. Trajectory Planning for Effective Close-Proximity Sensing with Agile Vehicles. [Doctoral Dissertation]. University of Florida; 2011. Available from: http://ufdc.ufl.edu/UFE0042697

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[1] [2]

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