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An optimal guidance method based on orbital element constraints
LI Chaobing, LYU Chunhong, SHANG Teng
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2018, (4): 321680 -321680 .  DOI: 10.7527/S1000-6893.2018.21680

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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