| 1 |
Yu J, Zhang H H, Li J, et al Autonomous takeoff scheme design for Chang’e-6 on the far side of the Moon Aerospace Control and Application 2024, 50 (6): 12.
|
| 2 |
Shearer C K, Mccubbin F M, Eckley S, et al Apollo next generation sample analysis (ANGSA): an Apollo participating scientist program to prepare the lunar sample community for Artemis Space science reviews 2024, 220 (6): 62.
doi: 10.1007/s11214-024-01094-x
|
| 3 |
He B Y, Shen H X, Peng Q B Manned lunar mission planning based on once low earth orbit and twice low lunar orbit rendezvous and dockings Journal of National University of Defense Technology 2020, 42 (6): 19.
|
| 4 |
Crues E Z, Gentile J, Carothers S, et al. Design, development, and use of a lunar lander simulation for NASA’s Artemis program[C]//IEEE Aerospace Conference, 2024. DOI: 10.1109/AERO58975.2024.10521400.
|
| 5 |
Zhou J P, Lu L, Li Z Y, et al Orbit design for manned lunar exploration: challenges and perspectives Acta Aerodynamica Sinica 2023, 41 (8): 1.
|
| 6 |
Cao P F, He B Y, Peng Q B, et al Hybrid and two-level optimization design of circumlunar free-return trajectory for manned lunar landing mission Journal of Astronautics 2017, 38 (4): 331.
|
| 7 |
He B Y, Li H Y, Zhou J P Rapid design of circumlunar free-return high accuracy trajectory and trans-lunar window for manned lunar landing mission Journal of Astronautics 2016, 37 (5): 512.
|
| 8 |
Zhou W M. Finite thrust orbit design for manned lunar prospecting series mission using inverse dynamics method[D]. Changsha: National University of Defense Technology, 2019. (in Chinese)
|
| 9 |
Yang L Y, Li H Y, Zhang J, et al Design and characteristic analysis for lunar module’s trans-lunar trajectory based on multi-conic method Journal of Astronautics 2019, 40 (12): 1383.
|
| 10 |
Qi Y, Xu S J Minimum delta V for the transfer to permanent lunar orbits with hyperbolic approach Acta Astronautica 2016, 119, 183.
doi: 10.1016/j.actaastro.2015.11.016
|
| 11 |
Qi Y, Xu S J Optimal earth-moon transfers using lunar gravity assist in the restricted four-body problem Acta Astronautica 2017, 134, 106.
doi: 10.1016/j.actaastro.2017.02.002
|
| 12 |
Filho L A G, Fernandes S D S Minimum fuel trajectories for round trip lunar missions Computational and Applied Mathematics 2018, 37 (3): 3608.
doi: 10.1007/s40314-017-0533-y
|
| 13 |
Filho L A G, Fernandes S D S Optimal round trip lunar missions based on the patched-conic approximation Computational and Applied Mathematics 2016, 35 (3): 753.
doi: 10.1007/s40314-015-0247-y
|
| 14 |
Filho L A G, Fernandes S D S A lunar flyby for a tridimensional Earth-to-Earth mission Acta Astronautica 2018, 151, 228.
doi: 10.1016/j.actaastro.2018.06.006
|
| 15 |
Tan M H, Ma B B, Shen H Energy analysis and optimizations of two-impulse Earth-Moon transfers in the Sun-Earth-Moon system Advance in Space Research 2022, 70 (8): 2369.
doi: 10.1016/j.asr.2022.07.028
|
| 16 |
Tselousova A, Shirobokov M, Trofimov S Direct two-impulse transfers from a Low-Earth Orbit to high circular polar orbits around the Moon AIP Conference Proceedings 2019, 2171 (1): 130022.
doi: 10.1063/1.5133289
|
| 17 |
Sandro D S F, Luiz A G F Optimal Earth-Moon trajectories in elliptic models: part 1 round-trip missions Journal of the Brazilian Society of Mechanical Sciences and Engineering 2021, 43 (12): 575.
doi: 10.1007/s40430-021-03281-1
|
| 18 |
Luiz A G F, Sandro D S F Optimal Earth-Moon trajectories in elliptic models: part 2 transfer between elliptic low earth orbit to elliptic low moon orbit Journal of the Brazilian Society of Mechanical Sciences and Engineering 2022, 44 (5): 217.
doi: 10.1007/s40430-022-03504-z
|
| 19 |
Lu L. Study on orbit schemes for manned lunar polar exploration missions[D]. Changsha: National University of Defense Technology, 2020. (in Chinese)
|
| 20 |
Lu L, Li H Y, Zhou W M, et al Design of earth-moon transfer orbit for manned lunar polar exploration missions Journal of Astronautics 2021, 42 (4): 425.
doi: 10.3873/j.issn.1000-1328.2021.04.003
|
| 21 |
Lu L, Li H Y, Dong T S, et al A fast calculation method for three-impulse contingency return trajectory during the near-moon phase based on differential algebra Chinese Journal of Aeronautics 2025, 38 (4): 103286.
doi: 10.1016/j.cja.2024.10.018
|
| 22 |
Yang L Y, Luo Y Z, Li H Y, et al. A fast solution to two-impulse lunar transfer trajectory based on machine learning method[C]//IEEE Congress on Evolutionary Computation (CEC) as part of the IEEE World Congress on Computational Intelligence (IEEE WCCI), 2020. DOI: 10.1109/CEC48606.2020.9185586.
|
| 23 |
Li H Y, Chen S Y, Izzo D, et al Deep networks as approximators of optimal low-thrust and multi-impulse cost in multitarget missions Acta Astronautica 2020, 166, 469.
doi: 10.1016/j.actaastro.2019.09.023
|
| 24 |
Yin S, Li J, Cheng L Low-thrust spacecraft trajectory optimization via a DNN-based method Advances in Space Research 2020, 66 (7): 1635.
doi: 10.1016/j.asr.2020.05.046
|
| 25 |
Guo X, Ren D, Wu D, et al DNN estimation of low-thrust transfer time: focusing on fast transfers in multi-asteroid rendezvous missions Acta Astronautica 2023, 204, 518.
doi: 10.1016/j.actaastro.2022.09.006
|
| 26 |
Izzo D, Sprague C I, Tailor D V. Machine learning and evolutionary techniques in interplanetary trajectory design[M]. Cham: Springer, 2019.
|
| 27 |
Li J H, Wang M Y, Chen W Y, et al Ballistic trajectory planning for midcourse interceptors based on convolutional neural networks Military Operations Research and Assessments 2023, 38 (6): 56.
|
| 28 |
Lu L, Li H Y, Dong T S Intelligent decision-making approach for contingency return trajectory based on production rule base and deep learning IEEE Trans. on Aerospace and Electronic Systems 2025, 61 (1): 900.
doi: 10.1109/TAES.2024.3449272
|
| 29 |
He B Y. Analysis approaches for precision reachable sets of manned lunar orbits using numerical continuation theory[D]. Changsha: National University of Defense Technology, 2017. (in Chinese)
|
| 30 |
Zhu H, Luo Y Z, Yang Z Analysis and design of phasing strategy for lunar orbit short rendezvous mission Manned Spaceflight 2017, 23 (1): 8.
|
| 31 |
Le J, Xu S J, Zhang C F Analysis of three orbital maneuver strategies in homing phase of rendezvous docking Aerospace Shanghai 2008, 25 (5): 37.
|
| 32 |
Yang L Y, Li H Y, Zhang J, et al Fast solution to the free return orbit’s reachable domain of the manned lunar mission by deep neural network Journal of Systems Engineering and Electronics 2024, 35 (2): 495.
doi: 10.23919/JSEE.2023.000117
|
| 33 |
Li H Y, Lu L, Li Z Y, et al. Manned lunar landing mission orbital integration design system, design methods, and electronic equipment: 202410566497.7[P]. 2024-06-07.
|