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Cooperative guidance method based on impact time and angle control
TANG Yang, ZHU Xiaoping, ZHOU Zhou, YAN Fei
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2022, (1): 324844 -324844 .  DOI: 10.7527/S1000-6893.2020.24844

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341