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Three-dimensional Guidance Law Accounting for Second-order Dynamics of Missile Autopilot
QU Pingping, ZHOU Di
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2011, (11): 2096 -2105 .  DOI: CNKI:11-1929/V.20110615.1322.004

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341