Cloud CubeSat Thermoelectric Cooler Controller System

Overview

During the summer of 2010, our team developed a thermoelectric cooler control system as part of the University of Maryland-Baltimore County and Goddard NASA Space Flight Center Radiation and Climate Branch Cloud CubeSat Project. Our control system was built for Dr. Vanderlei Martins of the University of Maryland-Baltimore County Physics Department. We implemented a unity gain, closed-loop feedback system that read from a temperature-measuring sub-system. The system was controlled by a combination of an integrator and gain compensation and included a current amplifier to drive the thermoelectric cooler. We used a less powerful thermoelectric cooler than the Marlow device housed on the Cloud CubeSat and a less accurate thermistor (rated for 1% error) to read the temperature of the cold plate of the cooler. The thermoelectric cooler reached the set-point temperature voltage corresponding to -30 degrees Celsius in approximately 50 seconds. To our best knowledge--limited by the accuracy of our measuring devices--we achieved a steady-state error within +/-0.1K. We included a manual outlining the suggested changes to adjust our control system to the Marlow thermoelectric cooler.


Related Links


NASA/Olin Image NASA/Olin Image
Olin/NASA Home
Olin Logo Olin Logo
Goddard Flight Center
NASA Logo NASA Logo
Goddard Flight Center

Copyright 2004-2010 Olin-NASA Research Group
Some content is Copyright other authors as noted
Website by Samantha Yang '13