Estimation of inertial characteristics of tumbling spacecraft using constant state filter
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DOI: 10.1016/j.asr.2017.03.032
Abstract: Abstract Reconstruction of dynamical parameters is one of the main challenges faced in the on-orbit servicing missions for defunct spacecraft. And the quaternion plays a major role in parameterizations of the dynamical model. In this… read more here.
Keywords: state; state filter; spacecraft; constant state ... See more keywords