Our goal was to design a system that would allow the Notre Dame Rocketry Team to measure the altitude, acceleration, orientation, and position of their rocket in real time during flights. It consisted of three main components: the Vehicle Module, the Relay Station Module, and the Ground Station Module. Together, they work to send a live stream of sensor data from the nose cone of the vehicle to a gound station that displays a real-time feed of the readings, in addition to saving the measurements locally on the rocket for later analysis. This system has been dubbed the Pressure, Orientation, and Tracking, Automated Telemetry Operation, or POTATO for short.
Brief description of our initial project idea and initial draft of our project goals and requirements
Detailed overview of our design. This document describes the detailed requirements for subsystems as well as the system as a whole
This contains the finalized project materials including a detailed overview of everything we worked on, code, board files, and other resources that could be useful if this project were to continue.
Dr. Chisum has acted as our advisor throughout the course of our project. His expertise in RF systems was indispensable in helping us design our project.
Alex worked on designing the Transceiver Board as well as writing the code to interface with the ADF chip.
Contact: afilmer@nd.eduMeghan worked on designing the Vehicle and Ground/Relay Station boards, in addition to writing the code for the IMU and accelerometer.
Contact: mfinnan@nd.eduMike worked on designing the Transceiver Board, and wrote the code to interface with the ADF chip, GPS, and altimeter.
Contact: mfrye@nd.eduZach integrated the various sensor code modules into the Vehicle Module code, and also helped design the Vehicle and Ground/Relay station boards.
Contact: zkowalcz@nd.eduTristen single-handedly designed the antennas used in this project.
Contact: tlewand1@nd.edu