Adaptive robust control of coupled attitude and orbit for spacecraft with model uncertainties
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DOI: 10.1108/aeat-07-2016-0113
Abstract: Purpose The purpose of this paper is to propose an adaptive robust controller for coupled attitude and orbit control of rigid spacecraft based on dual quaternion in the presence of external disturbances and model uncertainties.… read more here.
Keywords: model uncertainties; adaptive robust; attitude orbit; coupled attitude ... See more keywords