DOSS Satellite

Spacecraft name DOSS (Differential Optical Shadow Sensor CubeSat)
Form factor CubeSat
Units or mass 3U
Status cancelled
Organization University of Florida
Institution University
Entity Academic / Education
Country US
Partners Stanford University

Drag-free and attitude control design and simulation.


Drag-free and attitude control design and simulation, satellite bus development, and optimization of satellite constellation configuration for the determination of Earth’s geopotential and upper atmospheric winds and density.

Sources [1]

Last modified: 2024-05-29

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Created by Erik Kulu


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