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Strapdown stellar-inertial composite guidance method for ballistic missile considering the star sensor installation error
赵依 张洪波 汤国建
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 0, (): 0 -0 .  DOI: 10.7527/S1000-6893.2019.23603

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341