Deep networks as approximators of optimal low-thrust and multi-impulse cost in multitarget missions H Li, S Chen, D Izzo, H Baoyin
Acta Astronautica 166, 469-481, 2020
75 2020 J2-perturbed multitarget rendezvous optimization with low thrust H Li, S Chen, H Baoyin
Journal of Guidance, Control, and Dynamics 41 (3), 802-808, 2018
59 2018 Neural networks in time-optimal low-thrust interplanetary transfers H Li, H Baoyin, F Topputo
Ieee Access 7, 156413-156419, 2019
43 2019 Optimization of multiple debris removal missions using an evolving elitist club algorithm H Li, H Baoyin
IEEE Transactions on Aerospace and Electronic Systems 56 (1), 773-784, 2019
29 2019 Optimization for Multitarget, Multispacecraft Impulsive Rendezvous Considering S Chen, F Jiang, H Li, H Baoyin
Journal of Guidance, Control, and Dynamics 44 (10), 1811-1822, 2021
25 2021 An adaptive sampling method for Kriging surrogate model with multiple outputs Z Zhai, H Li, X Wang
Engineering with Computers, 1-19, 2020
24 2020 Multi-rendezvous low-thrust trajectory optimization using costate transforming and homotopic approach S Chen, H Li, H Baoyin
Astrophysics and Space Science 363, 1-16, 2018
22 2018 Power-limited low-thrust trajectory optimization with operation point detection Z Chi, H Li, F Jiang, J Li
Astrophysics and Space Science 363, 1-12, 2018
21 2018 Effects of superimposed pressure on the mechanical properties of HTPB propellant in a wide temperature range L Zhang, Z Shen, H Li
Propellants, Explosives, Pyrotechnics 45 (8), 1216-1226, 2020
19 2020 Autonomous time-optimal many-revolution orbit raising for electric propulsion GEO satellites via neural networks H Li, F Topputo, H Baoyin
arXiv preprint arXiv:1909.08768, 2019
19 2019 Cohesive zone model for mode-I fracture with viscoelastic-sensitivity HR Cui, HY Li, ZB Shen
Engineering Fracture Mechanics 221, 106578, 2019
18 2019 Dynamics and control for contactless interaction between spacecraft and tumbling debris H Li, J Li, F Jiang
Advances in Space Research 61 (1), 154-166, 2018
17 2018 A novel time dependent cohesive zone model for the debonding interface between solid propellant and insulation H Cui, Z Shen, H Li
Meccanica 53, 3527-3544, 2018
16 2018 Gtoc 11: Results from tsinghua university and shanghai institute of satellite engineering Z Zhang, N Zhang, X Guo, D Wu, X Xie, J Li, J Yang, S Chen, F Jiang, ...
Acta Astronautica 202, 819-828, 2023
15 2023 Deep networks as approximators of optimal transfers solutions in multitarget missions H Li, S Chen, D Izzo, H Baoyin
arXiv preprint arXiv:1902.00250, 2019
15 2019 Sequence optimization for multiple asteroids rendezvous via cluster analysis and probability-based beam search HY Li, HX Baoyin
Science China Technological Sciences 64 (1), 122-130, 2021
13 2021 A new constitutive equation for solid propellant with the effects of aging and viscoelastic Poisson’s ratio H Cui, Z Shen, H Li
Meccanica 53, 2393-2410, 2018
12 2018 Active disturbance rejection controller design for spacecraft attitude maneuver L Zhou, G Tang, H Li
Systems Engineering and Electronics 29 (12), 2122-2126, 2007
12 2007 General analysis method for global revisit characteristics of satellite constellation with repeating ground tracks X He, H Li
Acta Astronautica 202, 319-332, 2023
10 2023 An adaptive optimization algorithm based on clustering analysis for return multi-flight-phase of VTVL reusable launch vehicle J Zhao, X He, H Li, L Lu
Acta Astronautica 183, 112-125, 2021
8 2021 