Aerodynamic And Performance Analysis Of A Morphing Helicopter Rotor System,
2017
Embry-Riddle Aeronautical University
Aerodynamic And Performance Analysis Of A Morphing Helicopter Rotor System, Vinay Gopal Krishnan
Doctoral Dissertations and Master's Theses
The purpose of this study was to investigate the effect of rotor morphing, specifically variable rotor speed and variable blade twist, on various parameters such as the distribution of angle of attack, lift, power, thrust and/or other metrics describing the performance of a helicopter rotor. A MATLAB based blade element theory model was developed and executed for different flight conditions. The model was validated against the flight test data of a UH-60. Effects on power, lift to drag ratio and rotor drag from variations in blade twist, rotor speed, rotor radius and blade chord was analyzed. Morphing cases were applied …
A Study On The Control, Dynamics, And Hardware Of Micro Aerial Biomimetic Flapping Wing Vehicles,
2017
Embry-Riddle Aeronautical University
A Study On The Control, Dynamics, And Hardware Of Micro Aerial Biomimetic Flapping Wing Vehicles, Siara Hunt
Doctoral Dissertations and Master's Theses
Biological flight encapsulates 400 million years of evolutionary ingenuity and thus is the most efficient way to fly. If an engineering pursuit is not adhering to biomimetic inspiration, then it is probably not the most efficient design. An aircraft that is inspired by bird or other biological modes of flight is called an ornithopter and is the original design of the first airplanes. Flapping wings hold much engineering promise with the potential to produce lift and thrust simultaneously. In this research, modeling and simulation of a flapping wing vehicle is generated. The purpose of this research is to develop a …
Overview Of The Saber Mission And Launch Vehicle Design,
2017
University of Alabama in Huntsville
Overview Of The Saber Mission And Launch Vehicle Design, Benjamin Thompson, Jared Fuchs, Oakley Copeland, Aaron Hunt, Matthew Haskell, William Hankins, Logan Anderson
Von Braun Symposium Student Posters
No abstract provided.
Develop Pucp Microlab For Thinsat,
2017
Morehead State University
Develop Pucp Microlab For Thinsat, Robert J. Twiggs
Robert "Bob" Twiggs STEM Education Collection
A PowerPoint Presentation created by Professor Bob Twiggs titled "Develop PUCP microlab for ThinSat" from October 17, 2017.
Payloads For Student Thinsat Satellites,
2017
Morehead State University
Payloads For Student Thinsat Satellites, Robert J. Twiggs
Robert "Bob" Twiggs STEM Education Collection
A PowerPoint Presentation created by Professor Bob Twiggs titled "Payloads for Student ThinSat Satellites" from October 2, 2017.
The Shaping Of Things That Are: How Airplane Windows Took Their Shape,
2017
Embry-Riddle Aeronautical University
The Shaping Of Things That Are: How Airplane Windows Took Their Shape, Morgan Lopez
Student Works
Have you ever wondered why your airplane's windows are rounded? It is not for aesthetic appeal.
The first commercial jetliner windows' sole purpose was appearance; a squared window afforded an impressive view of the earth, but the view was not without consequence.
United States Drone Laws,
2017
Embry-Riddle Aeronautical University
United States Drone Laws, Jacob Crittenden
Student Works
The purpose of this Directed Study was to investigate and compile the drone laws that exist within the United States, both on the federal level and for each individual state. The federal laws are directed by the Federal Aviation Administration (FAA) under laws that pertain to “Unmanned Aircraft Systems” (UAS) and are relatively new. Most states have further regulations on UAS that they have passed. Most of these laws are in place to protect public safety and privacy, but some also prohibit certain locations of flight and certain modifications that might be made to the platform. State laws that limit …
Students Reaching For The Stars Become The Next Generation Of International Leaders,
2017
Morehead State University
Students Reaching For The Stars Become The Next Generation Of International Leaders, Robert J. Twiggs
Robert "Bob" Twiggs STEM Education Collection
A PowerPoint Presentation created by Professor Bob Twiggs titled "Students reaching for the stars become the next generation of International Leaders" on September 22, 2017.
Students Reaching For The Stars Become The Next Generation Of International Leaders: Pucp 100 Year Anniversary - Part 1,
2017
Morehead State University
Students Reaching For The Stars Become The Next Generation Of International Leaders: Pucp 100 Year Anniversary - Part 1, Robert J. Twiggs
Robert "Bob" Twiggs STEM Education Collection
A PowerPoint Presentation created by Professor Bob Twiggs titled "Students reaching for the stars become the next generation of International Leaders: PUCP 100 Year Anniversary" from September 22, 2017.
Students Reaching For The Stars Become The Next Generation Of International Leaders: Pucp 100 Year Anniversary - Part 2,
2017
Morehead State University
Students Reaching For The Stars Become The Next Generation Of International Leaders: Pucp 100 Year Anniversary - Part 2, Robert J. Twiggs
Robert "Bob" Twiggs STEM Education Collection
A PowerPoint Presentation created by Professor Bob Twiggs titled "Students reaching for the stars become the next generation of International Leaders: PUCP 100 Year Anniversary" from Saptember 22, 2017.
Unmanned Aerial Vehicle (Uav): Flight Performance,
2017
Embry-Riddle Aeronautical University
Unmanned Aerial Vehicle (Uav): Flight Performance, Fevens Louis Jean
Student Works
It is important that when measuring the sideslip angle and angles of attack during flight test performance of a UAV (Unmanned Aerial Vehicle), to fully understand that the Angles of attack and sideslip are parameters that aid in determining the safety of the flight as they improve stability and control of the aircraft. The disadvantage of the measurement of these angles using this method is low accuracy of measurement due to friction to the potentiometers in connection with the vanes. To counter this, a new sensing method was developed to minimize friction and collect more accurate data. The method is …
Tu-Pod: A Cube Satellite (Cubesat) And Tube Satellite Dispenser Produced Via 3d Printing, Successful Launch, Orbit And Dispensing Of Two Tube Satellites,
2017
Morehead State University
Tu-Pod: A Cube Satellite (Cubesat) And Tube Satellite Dispenser Produced Via 3d Printing, Successful Launch, Orbit And Dispensing Of Two Tube Satellites, Robert J. Twiggs, Matt Craft, Amin Djamshidpour, Chantal Cappelletti, Ken Biba, Stewart Davis
Robert "Bob" Twiggs STEM Education Collection
A PowerPoint Presentation created by Matt Craft, Amin Djamshidpour, Chantal Cappelletti, Bob Twiggs, Ken Biba, and Stewart Davis titled "TU-POD: A Cube Satellite (CubeSat) and Tube Satellite Dispenser Produced via 3D Printing, Successful Launch, Orbit and Dispensing of Two Tube Satellites" from August 6, 2017.
Using Unmanned Aerial Vehicles (‘Drones’) To Collect Data From Tagged Fishers In The Environment,
2017
California State University, Sacramento
Using Unmanned Aerial Vehicles (‘Drones’) To Collect Data From Tagged Fishers In The Environment, Vu A. Pham, Marc Horney, Aaron Drake
STAR Program Research Presentations
Fisher (Pekania pennant) belongs to the weasel family. In October 2014, the United States Fish and Wildlife Service proposed to list the West Coast Distinct Population Segment of fisher as threatened under the Endangered Species Act. We wish to better define where fishers live within their habitats and use that information to improve conservation efforts. Previously, to track the behavior of wild fishers, researchers put tracker collars on the animals and relied on networks of fixed antennas on the ground in the environment to collect data. We are experimenting with using unmanned aerial vehicles (‘drones’) to collect data …
Design, Development And Implementation Of Intelligent Algorithms To Increase Autonomy Of Quadrotor Unmanned Missions,
2017
Embry-Riddle Aeronautical University
Design, Development And Implementation Of Intelligent Algorithms To Increase Autonomy Of Quadrotor Unmanned Missions, Diego F. Garcia Herrera
Doctoral Dissertations and Master's Theses
This thesis presents the development and implementation of intelligent algorithms to increase autonomy of unmanned missions for quadrotor type UAVs. A six-degree-of freedom dynamic model of a quadrotor is developed in Matlab/Simulink in order to support the design of control algorithms previous to real-time implementation. A dynamic inversion based control architecture is developed to minimize nonlinearities and improve robustness when the system is driven outside bounds of nominal design. The design and the implementation of the control laws are described. An immunity-based architecture is introduced for monitoring quadrotor health and its capabilities for detecting abnormal conditions are successfully demonstrated through …
Providing A Unique Stem Education Opportunity With A Five-Day Eleo Mission,
2017
Morehead State University
Providing A Unique Stem Education Opportunity With A Five-Day Eleo Mission, Robert J. Twiggs
Robert "Bob" Twiggs STEM Education Collection
A PowerPoint Presentation created by Professor Bob Twiggs titled "Providing a Unique STEM Education Opportunity with a Five-Day ELEO Mission" from July 18, 2017.
Bringing Space To The Classroom Through Stem Education Providing Extreme Low Earth Orbit Missions Using Thinsats,
2017
Morehead State University
Bringing Space To The Classroom Through Stem Education Providing Extreme Low Earth Orbit Missions Using Thinsats, Robert J. Twiggs
Robert "Bob" Twiggs STEM Education Collection
An article written by Bob Twiggs and associates titled "Bringing Space to the Classroom Through STEM Education Providing Extreme Low Earth Orbit Missions Using ThinSats" from July 10, 2017.
Six Degrees Of Freedom From Six Degrees Of Separation: The History Of Flight Simulators,
2017
Embry-Riddle Aeronautical University
Six Degrees Of Freedom From Six Degrees Of Separation: The History Of Flight Simulators, David Keck, Morgan Lopez
Publications
Some of today's advanced flight simulators have the capacity to provide pilots with experiences of six degrees of freedom: forward/backward, up/down, or left/right (or pitching, rolling, or yawing in either direction). These incredible devices are the product of over 100 years of design developments that come from a series of technological discoveries and historical events.
Static Testing Of Propulsion Elements For Small Multirotor Unmanned Aerial Vehicles,
2017
Embry-Riddle Aeronautical University
Static Testing Of Propulsion Elements For Small Multirotor Unmanned Aerial Vehicles, Robert W. Deters, S.C. Kleinke, Michael S. Selig
Publications
The growing use of small multirotor aircraft has increased the interest in having better performance results especially with the propulsion system. The size of the propellers used on these aircraft operate at low Reynolds numbers that are typically less than 200,000. Static performance testing of ten propeller pairs (tractor and pusher) were completed and is the beginning of a systematic test of propellers used on multirotor systems. The propellers chosen for this initial set of tests were selected from four popular quadrotors. Besides testing the propellers provided with the aircraft, propellers that are sold as replacements from third-party companies were …
Wing Deflection Analysis Of 3d Printed Wind Tunnel Models,
2017
California Polytechnic State University, San Luis Obispo
Wing Deflection Analysis Of 3d Printed Wind Tunnel Models, Matthew G. Paul
Master's Theses
This work investigates the feasibility of producing small scale, low aerodynamic loading wind tunnel models, using FDM 3D printing methods, that are both structurally and aerodynamically representative in the wind tunnel. To verify the applicability of this approach, a 2.07% scale model of the NASA CRM was produced, whose wings were manufacturing using a Finite Deposition Modeling 3D printer. Experimental data was compared to numerical simulations to determine percent difference in wake distribution and wingtip deflection for multiple configurations.
Numerical simulation data taken in the form of CFD and FEA was used to validate data taken in the wind tunnel …
Deployable Antenna For Cubesat,
2017
California Polytechnic State University, San Luis Obispo
Deployable Antenna For Cubesat, Mackenzie Thomas Lennon, Caleb Andrew Barber, David Matthew Galves
Mechanical Engineering
This project is a proof-of-concept ground model of a large deployable antenna designed for the small space requirements of CubeSats. This small deployment module is designed to fit a 2 m by 1 m reflective antenna inside a storage volume of with the dimensions 20 cm by 20 cm x 40 cm. The reflector will be deployed to a parabolic shape with the goal of modeling the reflector necessary for high frequency communication. Because this module is designed as a proof-of-concept for the deployable parabolic reflector specifically, no electrical components will be incorporated and will just focus on the deployment …
