ESPRIT sun sensor: results and future use
Document ID: 323
Reichard, George1
Cochrane, Corey1
Student Papers
1 The Pennsylvania State University, Electrical Engineering Department, University Park, PA
Presented: 18th ESA Symposium on 'European Rocket and Balloon Programmes and Related Research'
Visby, Sweden, June 3-7, 2007
Abstract
A triple slit, digital sun sensor was designed for the ESPRIT rocket to gather sun angle data. lt was modeled after the sun sensor used for the Oscar-10 satellite because of its low cost and simplistic design. Based on the results, this sun sensor has proven to be an effective instrument aboard a spin stabilized payload.
Citation: | "ESPRIT sun sensor: results and future use", Reichard, G., C. Cochrane, Proceedings, 18th ESA Symposium on 'European Rocket and Balloon Programmes and Related Research', European Space Agency (ESA), November 2007, pp. 539 - 542 |