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Hidden-mode fault-tolerant spacecraft attitude estimation and control
Aviran Sadon
,
Daniel Choukroun
Department of Mechanical Engineering
Research output
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peer-review
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Keyphrases
Fault-tolerant
100%
Spacecraft Attitude Estimation
100%
Spacecraft Attitude Control
100%
Hidden Modes
100%
Monte Carlo Simulation
50%
Partial State Information
50%
Novel Design
50%
Simple System
50%
Design Approach
50%
Suboptimal Control
50%
Markov Jump Linear Systems
50%
Suboptimal Estimation
50%
Engineering
State Information
100%
Simple System
100%
Fault Mode
100%