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An iterative guidance algorithm using orbital elements as terminal constraints for spacecraft orbit transfer
DENG Yifan, LI Chaobing, WANG Zhigang
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2015, (6): 1975 -1982 .  DOI: 10.7527/S1000-6893.2015.0046

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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