The purpose of this project was to address the feasibility of retrofitting a four passenger private aircraft into an autonomous cargo transportation vehicle. A custom mechanical control mechanism prototype was developed that would replace a human pilot. The prototype developed addressed the three main controls on aircraft; roll, pitch and lift. Using knowledge of the selected aircraft configuration, the mechanical design each component was designed, analyzed to meet FAA guidelines and industry standards, and then constructed to demonstrate operation
This document outlines the design and implementation of a low-cost, low-power acceleration data reco...
Master of ScienceDepartment of Mechanical & Nuclear EngineeringDale SchinstockThis thesis describes ...
This Final Design Review report documents the senior project participating in the Vertical Flight So...
The purpose of this project was to design and fabricate an autonomous dirigible-based platform that ...
The goal of this project was to analyze, design and implement an autonomous quadrotor aerial vehicle...
This report contains the final developments and research involved with the modular biped robotic bas...
The purpose of this thesis is to conceptually design a fixed-wing unmanned aircraft systems (UAS) wi...
An Unmanned Aerial Vehicle (UAV) is a type of aircraft which can be driven without any pilot, crew ...
Presently wind tunnels are deployed to collect the majority of the experimental data on aerofoils an...
Flight testing continues to remain an essential step in the development or modification of an aircra...
The anticipated increase in rendezvous and docking activities in the various space programs in the S...
Thesis (M.S.) University of Alaska Fairbanks, 2021There has been an abundance of new and novel aircr...
The design will be an autonomous payload consisting of auto deployment of a drone running an autonom...
The purpose of this project was to update an existing ST5 Simulink Radio Frequency (RF) Communicatio...
The goal of this major qualifying project is to improve upon the search and rescue process with the ...
This document outlines the design and implementation of a low-cost, low-power acceleration data reco...
Master of ScienceDepartment of Mechanical & Nuclear EngineeringDale SchinstockThis thesis describes ...
This Final Design Review report documents the senior project participating in the Vertical Flight So...
The purpose of this project was to design and fabricate an autonomous dirigible-based platform that ...
The goal of this project was to analyze, design and implement an autonomous quadrotor aerial vehicle...
This report contains the final developments and research involved with the modular biped robotic bas...
The purpose of this thesis is to conceptually design a fixed-wing unmanned aircraft systems (UAS) wi...
An Unmanned Aerial Vehicle (UAV) is a type of aircraft which can be driven without any pilot, crew ...
Presently wind tunnels are deployed to collect the majority of the experimental data on aerofoils an...
Flight testing continues to remain an essential step in the development or modification of an aircra...
The anticipated increase in rendezvous and docking activities in the various space programs in the S...
Thesis (M.S.) University of Alaska Fairbanks, 2021There has been an abundance of new and novel aircr...
The design will be an autonomous payload consisting of auto deployment of a drone running an autonom...
The purpose of this project was to update an existing ST5 Simulink Radio Frequency (RF) Communicatio...
The goal of this major qualifying project is to improve upon the search and rescue process with the ...
This document outlines the design and implementation of a low-cost, low-power acceleration data reco...
Master of ScienceDepartment of Mechanical & Nuclear EngineeringDale SchinstockThis thesis describes ...
This Final Design Review report documents the senior project participating in the Vertical Flight So...