[FYP Log] Terrain Analysis System for a Picosatellite / CubeSat
This is meant to be an experimental log of my final year project, with the hopes of sharing and gaining ideas and knowledge with CEans here 😀 Though, I have no idea what are the implications of putting FYP info public before it is actually finished. Oh well, it's just a log 😉
So, what's my project about? Well, I was aiming to continue my imaging work from CanSat more seriously, so I thought of making a more sophisticated imaging system. This time, liasing with other students, it's for a CubeSat. Mostly categorized as a Picosatellite, they have a mass of under 1kg.
More info: <a href="https://en.wikipedia.org/wiki/CubeSat" target="_blank" rel="nofollow noopener noreferrer">Cubesat</a>
Objectives:
- Develop a small low cost, high resolution imaging system
- Combine images with onboard telemetry using "packets" and transmit via a digital downlink with a range between 500 m - 100 km
- Perform image processing techniques to stitch images and analyze terrain data
- Low altitude target. Since this is our university's first CubeSat, we still have a long way to go before putting the CubeSat into proper orbit. Our first testing height will be 500 m.
- COTS components will be used most of the time, though am evaluating the cost effective ones.
- Since SAR or similar forms wont be used, terrain analysis would not consist of 3D data. This might be compensated by stereo imaging though, if I feel like pursuing that 😛
- Hopefully with the nadir of the CubeSat perpendicular to the ground, the CMOS camera will autonomously take pictures, periodically. Once a picture has been successfully taken, it will be saved on the on board SD card.
- The image will then combined with telemetry data such as GPS and accelerometer readings. All this will be transferred to the data modem via a 115kbps UART connection. These processes are controlled via a microcontroller.
- The data modem will downlink the data to the ground station at maximum of 288kbps. This varies with distance and atmospheric conditions. Depending on how high the CubeSat is, a tracker might be needed. But, that is beyond the scope of part 1 of my FYP. Perhaps next semester. The ground station will perform the mosaicking of the images to make a larger image map. Edge detection (and/or another process) will be performed to analyze the soil condition for terrain analysis.
My FYP will be solely limited to the imaging system. For the actual CubeSat project, that is under the purview of other students. However, I am still closely tied with the communications and electrical aspects of it.