A high-accuracy constrained SINS/CNS tight integrated navigation for high-orbit automated transfer vehicles
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DOI: 10.1016/j.actaastro.2018.07.015
Abstract: Abstract High-accuracy and reliable autonomous navigation is increasingly crucial for automated transfer vehicles (ATV). This paper proposes a novel strapdown inertial navigation system/celestial navigation system (SINS/CNS) tight integration scheme aided by dynamic model constraints for… read more here.
Keywords: high orbit; accuracy; navigation; high accuracy ... See more keywords