Optical tracking and orbit determination performance of self-illuminated small spacecraft: LEDSAT (LED-based SATellite)
F Santoni, P Seitzer, T Cardona, G Locatelli… - Advances in Space …, 2018 - Elsevier
LEDSAT is a 1U CubeSat developed by S5Lab team of Sapienza–University of Rome in
collaboration with the Astronomy Department of University of Michigan. The main goal of the
mission is to demonstrate that a LED-based active illumination system may be used to
achieve orbit and attitude determination. LEDSAT will be placed into a Low Earth Orbit
(LEO) and observed by a network of ground-based telescopes. A LED-based system may
improve the accuracy in monitoring LEO spacecraft. A simple model is developed to …
collaboration with the Astronomy Department of University of Michigan. The main goal of the
mission is to demonstrate that a LED-based active illumination system may be used to
achieve orbit and attitude determination. LEDSAT will be placed into a Low Earth Orbit
(LEO) and observed by a network of ground-based telescopes. A LED-based system may
improve the accuracy in monitoring LEO spacecraft. A simple model is developed to …
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