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Development of an SE(3)-based Rigid Body Pose Estimation Scheme for Unknown Moments of Inertia in a Spacecraft

The objective of this proposal is the development of an SE(3)-based rigid body pose estimation scheme for unknown moments of inertia in a spacecraft. This estimator design will a) account for translation/rotation coupling, b) avoid singularity or non-uniqueness issues, c) gain high level of convergence, and d)account for system uncertainties.

Research Dates

05/05/2021 to 01/21/2022

Categories: Graduate