Location
Presentation- Allen E. Paulson College of Engineering and Computing
Document Type and Release Option
Thesis Presentation (Restricted to Georgia Southern)
Faculty Mentor
Valentin Soloiu
Faculty Mentor Email
vsoloiu@georgiasouthern.edu
Presentation Year
2021
Start Date
26-4-2021 12:00 AM
End Date
30-4-2021 12:00 AM
Keywords
Aicraft, sensors, collision detection
Description
Aircraft are one of the most used alternatives of traveling long distances and making them safer is a global necessity. For this reason, being able to create a functional prototype where the aircraft would be capable to acquire and process information in real time from the environment generating wingtip collision detection and simulation of a collection of exteroceptive sensors is necessary in progressing air flight safety systems. The aim of this project is to design and build an electronic aircraft undercarriage composed with multiple exteroceptive sensors that will be able to determine and process digital information of the aircraft envelope, and give an analytical output represented in different visuals and active commands in order to avoid obstacles for the aircraft. This will be achieved by the new concept of Wingtip Collision Detection developed in this thesis.
Academic Unit
Allen E. Paulson College of Engineering and Computing
Aircraft Runway Safe Navigation System
Presentation- Allen E. Paulson College of Engineering and Computing
Aircraft are one of the most used alternatives of traveling long distances and making them safer is a global necessity. For this reason, being able to create a functional prototype where the aircraft would be capable to acquire and process information in real time from the environment generating wingtip collision detection and simulation of a collection of exteroceptive sensors is necessary in progressing air flight safety systems. The aim of this project is to design and build an electronic aircraft undercarriage composed with multiple exteroceptive sensors that will be able to determine and process digital information of the aircraft envelope, and give an analytical output represented in different visuals and active commands in order to avoid obstacles for the aircraft. This will be achieved by the new concept of Wingtip Collision Detection developed in this thesis.
Comments
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