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Flying range control guidance for varying⁃speed missiles based on optimal error dynamics
Yuanhe LIU, Kebo LI, Shaoming HE, Yangang LIANG
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2023, (7): 326909 -326909 .  DOI: 10.7527/S1000-6893.2022.26909

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Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics

All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341