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You searched for subject:(Aircraft roll). Showing records 1 – 14 of 14 total matches.

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University of Florida

1. 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 October 20, 2019. http://ufdc.ufl.edu/UFE0024477.

MLA Handbook (7th Edition):

Grant, Daniel. “Modeling and Dynamic Analysis of a Multi-Joint Morphing Aircraft.” 2009. Web. 20 Oct 2019.

Vancouver:

Grant D. Modeling and Dynamic Analysis of a Multi-Joint Morphing Aircraft. [Internet] [Masters thesis]. University of Florida; 2009. [cited 2019 Oct 20]. 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

2. 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 October 20, 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. 20 Oct 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 Oct 20]. 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

3. Troner, David B. Aeroelastic Analysis of Wing Twist for Roll Control of a Micro Air Vehicle.

Degree: 2015, University of Florida

 With increasing growth of micro air vehicles and flexible aircraft structures, new ways to control aircraft are needed where conventional trailing edge control surfaces are… (more)

Subjects/Keywords: Aerodynamic lift; Aeroelasticity; Ailerons; Aircraft; Aircraft design; Aircraft roll; Aircraft wings; Stiffness; Structural deflection; Velocity; Aeroelasticity; aerodynamics; aircraft structures; micro air vehicle; wing twist

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APA (6th Edition):

Troner, D. B. (2015). Aeroelastic Analysis of Wing Twist for Roll Control of a Micro Air Vehicle. (Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/AA00038571

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

Chicago Manual of Style (16th Edition):

Troner, David B. “Aeroelastic Analysis of Wing Twist for Roll Control of a Micro Air Vehicle.” 2015. Thesis, University of Florida. Accessed October 20, 2019. http://ufdc.ufl.edu/AA00038571.

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

MLA Handbook (7th Edition):

Troner, David B. “Aeroelastic Analysis of Wing Twist for Roll Control of a Micro Air Vehicle.” 2015. Web. 20 Oct 2019.

Vancouver:

Troner DB. Aeroelastic Analysis of Wing Twist for Roll Control of a Micro Air Vehicle. [Internet] [Thesis]. University of Florida; 2015. [cited 2019 Oct 20]. Available from: http://ufdc.ufl.edu/AA00038571.

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

Council of Science Editors:

Troner DB. Aeroelastic Analysis of Wing Twist for Roll Control of a Micro Air Vehicle. [Thesis]. University of Florida; 2015. Available from: http://ufdc.ufl.edu/AA00038571

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


University of Florida

4. Lacroix, Bradley W. On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles.

Degree: PhD, Mechanical Engineering - Mechanical and Aerospace Engineering, 2013, University of Florida

 This document details the research performed on applying piezoelectric macro fiber composite actuators on micro air vehicles. The research objective was to apply the minimum… (more)

Subjects/Keywords: Aircraft; Aircraft pitch; Aircraft roll; Aircraft wings; Carbon fibers; Design optimization; Geometry; Steels; Swept wings; Wind tunnels; composite  – fiber  – flying  – macro  – materials  – mav  – mfc  – morphing  – optimization  – piezoelectric  – smart  – uav  – wing

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APA (6th Edition):

Lacroix, B. W. (2013). On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0046212

Chicago Manual of Style (16th Edition):

Lacroix, Bradley W. “On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles.” 2013. Doctoral Dissertation, University of Florida. Accessed October 20, 2019. http://ufdc.ufl.edu/UFE0046212.

MLA Handbook (7th Edition):

Lacroix, Bradley W. “On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles.” 2013. Web. 20 Oct 2019.

Vancouver:

Lacroix BW. On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2019 Oct 20]. Available from: http://ufdc.ufl.edu/UFE0046212.

Council of Science Editors:

Lacroix BW. On the Mechanics, Computational Modeling, and Design Implementation of Piezoelectric Actuators on Micro Air Vehicles. [Doctoral Dissertation]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0046212


University of Florida

5. Shields, Matthew C. A Model for Roll Stall and the Inherent Stability Modes of Low Aspect Ratio Wings at Low Reynolds Numbers.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2014, University of Florida

 The development of Micro Aerial Vehicles has been hindered by the poor understanding of the aerodynamic loading and stability and control properties of the low… (more)

Subjects/Keywords: Aerodynamics; Aircraft roll; Aircraft wings; Aspect ratio; Damping; Flat plates; Geometric angles; Sideslip; Stall; Winglets; aerodynamics  – lowaspectratiowings  – lowreynoldsnumber  – rollstall  – stabilityandcontrol  – windtunneltesting

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APA (6th Edition):

Shields, M. C. (2014). A Model for Roll Stall and the Inherent Stability Modes of Low Aspect Ratio Wings at Low Reynolds Numbers. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0045928

Chicago Manual of Style (16th Edition):

Shields, Matthew C. “A Model for Roll Stall and the Inherent Stability Modes of Low Aspect Ratio Wings at Low Reynolds Numbers.” 2014. Doctoral Dissertation, University of Florida. Accessed October 20, 2019. http://ufdc.ufl.edu/UFE0045928.

MLA Handbook (7th Edition):

Shields, Matthew C. “A Model for Roll Stall and the Inherent Stability Modes of Low Aspect Ratio Wings at Low Reynolds Numbers.” 2014. Web. 20 Oct 2019.

Vancouver:

Shields MC. A Model for Roll Stall and the Inherent Stability Modes of Low Aspect Ratio Wings at Low Reynolds Numbers. [Internet] [Doctoral dissertation]. University of Florida; 2014. [cited 2019 Oct 20]. Available from: http://ufdc.ufl.edu/UFE0045928.

Council of Science Editors:

Shields MC. A Model for Roll Stall and the Inherent Stability Modes of Low Aspect Ratio Wings at Low Reynolds Numbers. [Doctoral Dissertation]. University of Florida; 2014. Available from: http://ufdc.ufl.edu/UFE0045928


University of Florida

6. Thompson, Rhoe. Haltere Mediated Flight Stabilization in Diptera Rate Decoupling, Sensory Encoding, and Control Realization.

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

 Insects of the order Diptera have a single pair of wings. The rear wings of Dipteran insects have evolved into organs that allow stabilizing control… (more)

Subjects/Keywords: Aircraft pitch; Aircraft roll; Aircraft wings; Damping; Insects; Kinematics; Sensilla; Simulations; Trajectories; Yaw rotation; campaniform, control, coriolis, df2, diptera, dynamics, encoding, flight, gyroscope, haltere, imu, saccade, sensilla, stabilization

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APA (6th Edition):

Thompson, R. (2009). Haltere Mediated Flight Stabilization in Diptera Rate Decoupling, Sensory Encoding, and Control Realization. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0024793

Chicago Manual of Style (16th Edition):

Thompson, Rhoe. “Haltere Mediated Flight Stabilization in Diptera Rate Decoupling, Sensory Encoding, and Control Realization.” 2009. Doctoral Dissertation, University of Florida. Accessed October 20, 2019. http://ufdc.ufl.edu/UFE0024793.

MLA Handbook (7th Edition):

Thompson, Rhoe. “Haltere Mediated Flight Stabilization in Diptera Rate Decoupling, Sensory Encoding, and Control Realization.” 2009. Web. 20 Oct 2019.

Vancouver:

Thompson R. Haltere Mediated Flight Stabilization in Diptera Rate Decoupling, Sensory Encoding, and Control Realization. [Internet] [Doctoral dissertation]. University of Florida; 2009. [cited 2019 Oct 20]. Available from: http://ufdc.ufl.edu/UFE0024793.

Council of Science Editors:

Thompson R. Haltere Mediated Flight Stabilization in Diptera Rate Decoupling, Sensory Encoding, and Control Realization. [Doctoral Dissertation]. University of Florida; 2009. Available from: http://ufdc.ufl.edu/UFE0024793


University of Florida

7. 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 October 20, 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. 20 Oct 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 Oct 20]. 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

8. 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 October 20, 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. 20 Oct 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 Oct 20]. 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

9. Babcock, Judson T. Aeroservoelastic Design for Closed-Loop Flight Dynamics of a MAV.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2013, University of Florida

 Some fixed-wing micro air vehicles (MAVs) have high levels of structural flexibility, a property which can change the flight dynamics and control characteristics of the… (more)

Subjects/Keywords: Aircraft; Aircraft roll; Aircraft wings; Bending; Damping; Flight dynamics; Gusts; Natural frequencies; Stiffness; Structural deflection; aeroelastic  – aeroelasticity  – aeroservoelasticity  – aswing  – closed-loop  – elastic-axis  – flight-control  – flight-dynamics  – gust  – lqr  – micro-air-vehicle  – stiffness

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APA (6th Edition):

Babcock, J. T. (2013). Aeroservoelastic Design for Closed-Loop Flight Dynamics of a MAV. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0045699

Chicago Manual of Style (16th Edition):

Babcock, Judson T. “Aeroservoelastic Design for Closed-Loop Flight Dynamics of a MAV.” 2013. Doctoral Dissertation, University of Florida. Accessed October 20, 2019. http://ufdc.ufl.edu/UFE0045699.

MLA Handbook (7th Edition):

Babcock, Judson T. “Aeroservoelastic Design for Closed-Loop Flight Dynamics of a MAV.” 2013. Web. 20 Oct 2019.

Vancouver:

Babcock JT. Aeroservoelastic Design for Closed-Loop Flight Dynamics of a MAV. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2019 Oct 20]. Available from: http://ufdc.ufl.edu/UFE0045699.

Council of Science Editors:

Babcock JT. Aeroservoelastic Design for Closed-Loop Flight Dynamics of a MAV. [Doctoral Dissertation]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0045699


Brigham Young University

10. Paulsen, Trevor H. Low Cost/ High Precision Flight Dynamics Estimation Using the Square-Root Unscented Kalman Filter.

Degree: MS, 2009, Brigham Young University

 For over a decade, Brigham Young University's Microwave Earth Remote Sensing (MERS) team has been developing SAR systems and SAR processing algorithms. In order to… (more)

Subjects/Keywords: SR-UKF; UKF; aircraft; flight; dynamics; Kalman; filter; GPS; accelerometer; gyroscope; airplane; tracking; SAR; motion; processing; sensor; IMU; MATLAB; roll; pitch; yaw; MOTRON; UAV; unscented; Electrical and Computer Engineering

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APA (6th Edition):

Paulsen, T. H. (2009). Low Cost/ High Precision Flight Dynamics Estimation Using the Square-Root Unscented Kalman Filter. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=2921&context=etd

Chicago Manual of Style (16th Edition):

Paulsen, Trevor H. “Low Cost/ High Precision Flight Dynamics Estimation Using the Square-Root Unscented Kalman Filter.” 2009. Masters Thesis, Brigham Young University. Accessed October 20, 2019. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=2921&context=etd.

MLA Handbook (7th Edition):

Paulsen, Trevor H. “Low Cost/ High Precision Flight Dynamics Estimation Using the Square-Root Unscented Kalman Filter.” 2009. Web. 20 Oct 2019.

Vancouver:

Paulsen TH. Low Cost/ High Precision Flight Dynamics Estimation Using the Square-Root Unscented Kalman Filter. [Internet] [Masters thesis]. Brigham Young University; 2009. [cited 2019 Oct 20]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=2921&context=etd.

Council of Science Editors:

Paulsen TH. Low Cost/ High Precision Flight Dynamics Estimation Using the Square-Root Unscented Kalman Filter. [Masters Thesis]. Brigham Young University; 2009. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=2921&context=etd


University of Florida

11. 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 October 20, 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. 20 Oct 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 Oct 20]. 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

12. 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 October 20, 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. 20 Oct 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 Oct 20]. 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

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

13. Rao, Arjun. Measurement of aerodynamic characteristics of MAVs using motion tracking.

Degree: MS, 4048, 2012, University of Illinois – Urbana-Champaign

 Aerodynamic characteristics of Micro Air Vehicles (MAVs) is not well addressed in aeronautics literature, and more experimental data are required to help better understand the… (more)

Subjects/Keywords: Micro air vehicle (MAV); Reynolds number; remote controlled (RC); aircraft; airplane; model; Lift; drag; thrust; moment; stability; control; pitch; roll; yaw; weathercock; weathervane; motion tracking; motion capture; VICON; camera; wand; Re; lift curve; drag polar; propeller; Advanced Precision Composites (APC); sport; E-flite; sideslip; static margin (SM); axis; axes; PropellerScanner; airfoil; wing; lifting line theory; theory; experimental; Aerodynamics; calibration; noise; markers; camera; Euler angles; longitudinal; lateral; advance ratio; density; data points; Extra 260; Extra 300 3D; glider; frequency; revolutions per minute (RPM); body-fixed; Earth-fixed; transformation; rotation; matrix; filter; low-pass; finite difference; robust; lineqar; least-squares; parabolic; Uhlig; Selig; Rao

…The Vicon markers built into separate objects with the propeller, the aircraft, and the two… …position time history of the stationary aircraft… …Histogram for the attitude time history of the stationary aircraft… …Glide path of aircraft for six different repeatability tests… …Repeatability tests for aircraft position track… 

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APA (6th Edition):

Rao, A. (2012). Measurement of aerodynamic characteristics of MAVs using motion tracking. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/30943

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

Chicago Manual of Style (16th Edition):

Rao, Arjun. “Measurement of aerodynamic characteristics of MAVs using motion tracking.” 2012. Thesis, University of Illinois – Urbana-Champaign. Accessed October 20, 2019. http://hdl.handle.net/2142/30943.

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

MLA Handbook (7th Edition):

Rao, Arjun. “Measurement of aerodynamic characteristics of MAVs using motion tracking.” 2012. Web. 20 Oct 2019.

Vancouver:

Rao A. Measurement of aerodynamic characteristics of MAVs using motion tracking. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2012. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/2142/30943.

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

Council of Science Editors:

Rao A. Measurement of aerodynamic characteristics of MAVs using motion tracking. [Thesis]. University of Illinois – Urbana-Champaign; 2012. Available from: http://hdl.handle.net/2142/30943

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

14. Lederman, Jerusha Isabel. Dynamics in the Anvil Outflow of Tropical Convection.

Degree: PhD, Earth & Space Science, 2015, York University

 This thesis presents results of an experiment to investigate the dynamics of air motions within the outflow of tropical deep convection in the upper troposphere… (more)

Subjects/Keywords: Atmospheric sciences; Physics; Meteorology; Isolated wave; Isolated waves; Gravity wave; Gravity waves; Deep convection; Convective roll; Horizontal convective roll; HCR; Convective rolls; Anvil; Cirrus; Cirrus clouds; Anvil outflow; Aircraft safety; Thunderstorm no fly zone; Plane; Planes; Flight hazard; Rayleigh-Benard convection; Rayleigh-Benard; Rankine vortex; Outflow; Convection; Tropical; Tropical convection; Maritime continent; Tropopause; Troposphere; Upper Troposphere Lower Stratosphere; UTLS; Atmosphere; Atmospheric dynamics; Dynamics; Instability; Instabilities; Physics; Atmospheric physics; EMERALD; EMERALD 2; Experimental; Campaign; Airborne; Aircraft; Measurement; Measurements; Egrett; King Air; Turbulence; Jerusha; Jerusha Lederman; Lederman; Jim; Whiteway; Jim Whiteway; Storm; Tropical storm; Hector; Darwin; Australia; Tiwi Islands; Bathurst Island; Melville Island; Islands; Sea-breeze circulation; Small scale dynamics; Lidar; Radar; BAT probe; Turbulence probe; Light detection and ranging; Meteorology; Planetary science; Science; Laser; Experiment; Stratified turbulence; Mammatus; Mammatus clouds; Mamma; Thunderstorm; Latent heat; Water vapor; Vapor; Vapour; Climate; Mixing; Air; Air motions; Waves; Wavelet; Wavelets; Dynamic; Analysis; Vertical velocity; Perturbation wind velocity; Perturbation vertical velocity; Potential temperature; Correlations; Wind temperature correlation; Phase; Phase relationship; Quasi-2d turbulence

…53 Figure 3.1: The Egrett aircraft outfitted with the suite of instruments for the EMERALD… …59 Figure 3.4: (a) BAT probe mounted on the left wing of the Egrett aircraft… …x28;b) Rosemount turbulence probe mounted on the right wing of the Egrett aircraft… …around the cirrus outflow region of an anvil cloud. Another campaign with the Egrett aircraft… …objectives were to 9 position the aircraft within the anvil outflow from deep tropical convection… 

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

APA (6th Edition):

Lederman, J. I. (2015). Dynamics in the Anvil Outflow of Tropical Convection. (Doctoral Dissertation). York University. Retrieved from http://hdl.handle.net/10315/30028

Chicago Manual of Style (16th Edition):

Lederman, Jerusha Isabel. “Dynamics in the Anvil Outflow of Tropical Convection.” 2015. Doctoral Dissertation, York University. Accessed October 20, 2019. http://hdl.handle.net/10315/30028.

MLA Handbook (7th Edition):

Lederman, Jerusha Isabel. “Dynamics in the Anvil Outflow of Tropical Convection.” 2015. Web. 20 Oct 2019.

Vancouver:

Lederman JI. Dynamics in the Anvil Outflow of Tropical Convection. [Internet] [Doctoral dissertation]. York University; 2015. [cited 2019 Oct 20]. Available from: http://hdl.handle.net/10315/30028.

Council of Science Editors:

Lederman JI. Dynamics in the Anvil Outflow of Tropical Convection. [Doctoral Dissertation]. York University; 2015. Available from: http://hdl.handle.net/10315/30028

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