AIAA Hybrid Rocket: Launch and Flight Control System 2019-20
C
C#
Python
Embedded Systems
FPGA
Enclosure
The purpose of this project is to design and implement a launch and flight control system to expand the capabilities of Oregon State's Hybrid Rocket team. A hybrid rocket uses both a solid fuel and liquid oxidizer allowing for a safer and more controlled motor burn. This presents a number of challenges not found on other university rocketry teams such as pre-flight remote oxidizer filling, ignition timing with oxidizer injection, mid-flight oxidizer flow control, and real-time video monitoring. It is for these reasons that we aim to create a safe, reliable, and expandable launch and flight control platform with robust hardware and software components that can be used by Hybrid teams for years to come.
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Artifacts
Name | Description | |
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GUI GitHub | This is a link to the repository housing all of the code for the GUI and its installer | Link |
Control Firmware GitHub | This is a link to the repository for the embedded firmware running on the Warp Core | Link |
Project Summary Video | This video provides an overview of our Launch and Flight Control module and outlines our accomplishments over the last three terms | Link |
Google Site link | This is the link to our team's website. The site provides assess to videos of our subscale tests and much more related to our project. | Link |
2018-2019 Launch of Nova Alas | A video of the launch of the 2018-2019 Hybrid Rocket, Nova Alas in Brothers, Oregon. | Link |
Motor Testing Compilation | A compilation of our static motor testing efforts this year | Link |
File Repository | This is a copy of some select items from our team-wide drive, relating to highlights from the project and the course. | Link |
Zoom Link | This link is used to join our June 5th Engineering Expo Zoom meeting | Link |