Model predictive and reallocation problem for CubeSat fault recovery and attitude control

Mechanical Systems and Signal Processing(2018)

Cited 20|Views6
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Abstract
•Innovative fault-tolerant algorithm for attitude control with magnetic torquers.•Model Predictive Control applied to a CubeSat mission.•Autonomous fault recovery without hot or cold redundancies.•Algorithm is adaptable from CubeSat to flagship missions.
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Key words
CubeSat,Model Predictive Control,Recovery,Attitude control,Magnetic torquers fault
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