Velocity and position error compensation using strapdown inertial navigation system/celestial navigation system integration based on ensemble neural network

DOI10.1016/J.AST.2007.08.005zbMath1273.70045OpenAlexW2035683930MaRDI QIDQ2853510

Fan Xu, Jiancheng Fang

Publication date: 22 October 2013

Published in: Aerospace Science and Technology (Search for Journal in Brave)

Full work available at URL: http://www.sciencedirect.com/science/article/pii/S127096380700106X

zbMATH Keywords

Kalman filtertransition matrixensemble neural networkintegrated navigationSINSCNS

Mathematics Subject Classification ID

Neural networks for/in biological studies, artificial life and related topics (92B20) Orbital mechanics (70M20)

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