李海阳

期刊论文

1. 吴伟静，李海阳，申志彬，刘钊宇（2026）. 基于力热能量密度等效原理的推进剂拉伸屈服强度率温相关性表征. 《推进技术》.
2. 黄嘉达，李海阳，申志彬，马浩（2026）. 基于区域物理加权U-Net模型的固体火箭发动机药柱应力应变场预测. 《推进技术》.
3. 吴栋，聂志杰，雷勇军，申志彬，李海阳，张大鹏（2026）. NEPE推进剂加压固化过程的非线性黏弹性本构模型及其应用. 《力学学报》.
4. 杜振江，李海阳，陆林，杨震，郭祥（2026）. 地月自由返回轨道出发可控域模型及特性分析. 《宇航学报》.
5. 常笑宽，李海阳，李泽越（2026）. 基于神经网络的地月转移中途修正脉冲快速估计方法. 《中国空间科学技术(中英文)》.DOI
6. Binyu Zhu, Haiyang Li, Zeyue Li, Jiyuan Lv (2026). Lunar Orbit Insertion Optimization Method Based on Retargeting Impulsive Controllable Set Features. Journal of Guidance Control and Dynamics.DOI
7. Heng Jing, Zhenjiang Du, Hailian Zhang, Binyu Zhu, Hua Wang, Haiyang Li (2026). Energy-level-constrained sequential lunar gravity assist trajectory replanning for trans-lunar injection failures. Aerospace Science and Technology.DOI
8. Xiaokuan Chang, Haiyang Li, Hailian Zhang, Xiang Guo, Xinwei Guo, Luyi Yang (2026). Design and analysis of Halo orbit constellations for navigation in the ERTBP. Advances in Space Research.DOI
9. Zhenjiang Du, Haiyang Li (2026). A fast calculation method for the controllable set of Earth–Moon free-return trajectories based on interval analysis. Aerospace Science and Technology.DOI
10. Zhenjiang Du, Heng Jing, Haiyang Li, Hua Wang (2026). Fast approximation and analysis for time-dependent controllable set of Earth–Moon transfer orbits via velocity surfaces method. Celestial Mechanics and Dynamical Astronomy.DOI
11. Zhenjiang Du, Haiyang Li, Hua Wang, Heng Jing (2026). Time-dependent controllable set for contingency return trajectories under spatiotemporal constraints in CR3BP. Aerospace Science and Technology.DOI
12. Zhenjiang Du, Heng Jing, Haiyang Li, Hua Wang (2026). Design and analysis of controllable domain for point return orbits using velocity surfaces. Advances in Space Research.DOI
13. Heng Jing, Zhenjiang Du, Haiyang Li, Hua Wang, Junhua He, Chengyi Huo (2026). Study on the reachable domain of Earth–Moon transfer orbits with terminal constraints in the CR3BP. Acta Astronautica.DOI
14. 张焘，李海阳，申志彬，吴国夫，卞云龙，王立民（2025）. 光纤光栅传感器在固体发动机药柱内部应变监测中的应用. 《国防科技大学学报》.
15. 邓旷威，李海阳，申志彬（2025）. HTPB推进剂拉压不对称黏弹塑性本构模型. 《国防科技大学学报》.
16. 朱彬羽，李海阳，杨震，何俊华，陆林，张宇航（2025）. 融合动力学特征的自由返回轨道双路网络学习方法. 《国防科技大学学报》.
17. 李道奎，孙海涛，周仕明，申志彬，李海阳，梁彦刚（2025）. 赛教融合的基础力学教学改革与实践. 《力学与实践》.
18. 王海涛，李海阳，梁彦刚，王华，周剑勇，张梦樱，张凡榛，黎克波，许鑫鑫（2025）. 理论力学实验课程建设实践与教学探索. 《大学教育》.
19. 张梦樱，梁彦刚，李海阳，王华（2025）. “理实结合，重数固基”的理论力学教学尝试. 《中国力学大会-2025摘要集（第一册）》.DOI
20. 张慧慧，赵汝岩，申志彬，李海阳（2025）. 高能推进剂细观结构损伤演化的定量表征. 《中国力学大会-2025论文集》.DOI
21. 张慧慧，赵汝岩，申志彬，李海阳（2025）. 高能推进剂细观结构损伤演化定量表征. 《中国力学大会-2025摘要集（第二册）》.DOI
22. 伏立峰，朱阅訸，李海阳（2025）. 非合作航天器意图识别的机器学习方法. 《火力与指挥控制》.
23. Binyu Zhu, Haiyang Li, Lin Lu, Zhenjiang Du, Luyi Yang (2025). Data and knowledge dual-driven design method for Earth–Moon free-return orbit. Aerospace Science and Technology.DOI
24. Xinwei Guo, Zhen-Jiang Du, Xiang Guo, Haiyang Li (2025). High-Fidelity Lunar Free-Return Trajectory Optimization via Neural Network and ATK Software. Journal of Physics Conference Series.DOI
25. Zhe-Xi Xue, Zhen-Jiang Du, Haiyang Li (2025). Controllable set model and characteristic analysis of long-distance guidance segment for earth departure circumlunar rendezvous. Journal of Physics Conference Series.DOI
26. Wen Luo, Jin Zhang, Shengxi Li, Xinyi Zi, Haiyang Li (2025). Real-time optimal exclusive angle determination method for IGSO communication satellite. Journal of Physics Conference Series.DOI
27. Zeyue Li, Haiyang Li, Haiyang Li, Zhen Yang, Jiyuan Lv (2025). Academy Transaction Note “non-smooth characteristics in uncertainty propagation for midcourse correction of Earth-Moon transfer orbit”. Acta Astronautica.DOI
28. Luyi Yang, Haiyang Li, Jin Zhang, Yuehe Zhu (2024). 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, Vol. 35, No. 2.DOI
29. 卞云龙，李海阳，申志彬，朱洪兵，王志强（2024）. 烧蚀对脉冲发动机软质隔层打开过程影响的试验设计. 《国防科技大学学报》.
30. 李海阳，张梦樱，周剑勇，王海涛（2024）. “文化为基、术业为干”的力学系列课程思政建设. 《第五届全国航空航天类课程思政教学改革论坛论文集（下）》.DOI
31. 王华，张元媛，李海阳（2024）. “航天系统仿真”课程案例设计与思政融入——以空间站交会为例. 《第五届全国航空航天类课程思政教学改革论坛论文集（下）》.DOI
32. 申志彬，邓旷威，李海阳，张慧慧（2024）. 长期贮存发动机中HTPB推进剂老化特性及蠕变本构模型. 《推进技术》.
33. 张慧慧，李海阳，申志彬（2024）. 考虑温度与围压的HTPB固体推进剂细观结构损伤演化机制. 《固体火箭技术》.
34. 王华，周晚萌，李海阳，杨震（2024）. 复杂轨道机动规划本体元模型与软件实现. 《宇航学报》.
35. 张梦樱，梁彦刚，李海阳，王华（2024）. “理实结合,AI赋能”:数字化转型下的“理论力学”教学实践与探索. 《第六届全国高等学校航空航天类专业教育教学研讨会》.DOI
36. 李泽越，杨震，李海阳，罗亚中（2024）. 航天器轨道机动自适应逆向移动滑窗检测方法. 《国防科技大学学报》.
37. 李泽越，李海阳，杨震（2024）. 时间约束松弛的载人月球探测轨道一体化设计方法. 《2024年中国航天大会论文集》.DOI
38. Jie Hu, Haiyang Li, Chen Xia, Zhaoqiang Xia (2024). Analysis of multi-photon quantum radar cross section for targets in atmospheric medium. Quantum Information Processing.DOI
39. Lin Lü, Haiyang Li, Tianshan Dong, Wanmeng Zhou (2024). A fast calculation method for three-impulse contingency return trajectory during the near-moon phase based on differential algebra. Chinese Journal of Aeronautics.DOI
40. Lin Lu, Haiyang Li, Tian-shan Dong (2024). Intelligent Decision-Making Approach for Contingency Return Trajectory Based on Production Rule Base and Deep Learning. IEEE Transactions on Aerospace and Electronic Systems.DOI
41. Lin Lu, Haiyang Li, Tianshan Dong, Binyu Zhu (2024). Design approach of contingency point return trajectory for manned lunar missions based on homotopy continuation. Journal of Physics Conference Series.DOI
42. Luyi Yang, Haiyang Li, Jin Zhang (2024). An interval programming method of earth-moon trajectory for manned lunar exploration mission under interval uncertainty. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
43. Zeyue Li, Haiyang Li, Zhen Yang (2024). Non-Smooth Deviation Evolution Analysis in Cislunar Midcourse Correction Trajectory Under Maneuver Execution Threshold.DOI
44. Zeyue Li, Zhen Yang, Haiyang Li, Wanmeng Zhou (2024). Integrated Orbital Design Method for Manned Lunar Exploration with Relaxed Temporal Constraints. Journal of Spacecraft and Rockets.DOI
45. 郭宇，申志彬，李海阳，张漩，李志杰（2023）. 长贮过程中发动机HTPB推进剂老化机理分析. 《国防科技大学学报》.
46. 卞云龙，李映坤，徐洁，李海阳，吴国夫（2023）. 脉冲固体火箭发动机软质隔层大变形特性研究. 《弹道学报》.
47. 李海阳，王华，张梦樱，周剑勇，梁彦刚（2023）. 基于CSE思想的力学系列课程改革研究. 《第五届全国高等学校航空航天类专业教育教学研讨会》.DOI
48. 张梦樱，梁彦刚，李海阳，王海涛，王华（2023）. 航天力学拔尖班“动力学与控制”贯通课探索. 《第五届全国高等学校航空航天类专业教育教学研讨会论文集》.
49. 杨路易，张海联，彭祺擘，李海阳，武新峰（2023）. 不同升降轨返回方式下定点返回轨道窗口解析分析方法. 《航空学报》.
50. 李泽越，李海阳，杨震，彭祺擘（2023）. 探月自由返回轨道设计的自适应初值Newton-Raphson方法. 《航空学报》.
51. 王奇，陆林，李海阳，杨路易（2023）. 基于可控域的定点返回轨道全局敏感性分析. 《系统工程与电子技术》.
52. 王华，吕纪远，李海阳（2023）. 载人月球探测序列任务组合仿真设计与试验. 《宇航学报》.
53. 周建平，陆林，李泽越，彭祺擘，李海阳（2023）. 载人月球探测轨道设计的挑战与技术发展趋势. 《空气动力学学报》.
54. 朱彬羽，李海阳，陆林，李兴永，周晚萌（2023）. 一种面向旋转空间站的绕月双曲交会导引控制方法. 《宇航学报》.
55. Jie Hu, Haiyang Li, Chen Xia (2023). Calculation and analysis of quantum radar scattering characteristics of targets in atmospheric medium. Optics Express.DOI
56. Haiyang Li, Zehua Liang, Qian-Wei Chen, Wei-Bo Huang, Hao Fu, Xiaoyue Lu (2023). Wide-band Pulsed Travelling Wave Tube Amplifier of Kilowatt Scale for Space Application. International Vacuum Electronics Conference.DOI
57. Jing Huang, Cheng Qiu, Yanhui You, Haiyang Li (2023). Intelligent Dynamic Force Loading Algorithm for Aerospace Rudder Load Simulator. Journal of Aerospace Engineering.DOI
58. Tangpei Jiao, Peng Chen, Haiyang Li, Wei-Bo Huang, Qianwen Chen, Hao Fu (2023). Space Pulsed Terahertz Traveling Wave Tube Amplifier. International Vacuum Electronics Conference.DOI
59. Chuntao Li, Haiyang Li, Weijing Wu, Wei Li, Aimin Pang (2023). Uniaxial tensile mechanical behavior research of HTPB propellant under wide temperature and confining pressure. AIP Advances.DOI
60. Yunlong Bian, Zhibin Shen, Haiyang Li, Weijing Wu, Tao Zhang, Guofu Wu, Hongbing Zhu (2023). Working process and opening characteristics of soft insulator of pulse motor. Propellants Explosives Pyrotechnics.DOI
61. Lin Lu, Jianping Zhou, Haiyang Li, Hailian Zhang (2023). Investigation on reachable domain of contingency return trajectories in the circumlunar flight phase based on interval analysis. Advances in Space Research.DOI
62. Lin Lu, Jianping Zhou, Haiyang Li, Qibo Peng, Wanmeng Zhou (2023). Study on controllable set of contingency return trajectories for crewed lunar missions based on interval analysis. Acta Astronautica.DOI
63. Luyi Yang, Haiyang Li, Xingyong Li, Zeyue Li, Lin Lu (2023). A Reinforcement Learning Method to Trajectory Design for Manned Lunar Mission via Reshaping Rewards. Lecture notes in electrical engineering.DOI
64. 郭宇，申志彬，孙翔宇，李海阳，周伟勇（2022）. 固体火箭发动机故障诊断技术现状及发展思考. 《固体火箭技术》.
65. 郭宇，李海阳，申志彬，汪根来，卞云龙（2022）. 固体火箭发动机橡胶密封结构可靠性试验及评估方法. 《固体火箭技术》.
66. 李海阳，梁彦刚，周剑勇，王海涛，张梦樱，张凡榛（2022）. 遥感与导航中的运动学原理虚拟仿真实验建设. 《第三届全国高等学校航空航天类专业教育教学研讨会》.
67. 赵建磊，李海阳（2022）. 稀疏轨道信息下的非合作飞行器机动识别方法. 《系统工程与电子技术》.
68. 卞云龙，李映坤，李海阳，申志彬，吴国夫（2022）. 双脉冲发动机Ⅰ脉冲工作过程中EPDM隔层烧蚀特性. 《固体火箭技术》.
69. Lin Lu, Jianping Zhou, Haiyang Li, Hailian Zhang (2022). Design of contingency point return trajectory in the lunar orbit insertion phase for crewed lunar exploration missions. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
70. Xiangyue He, Haiyang Li (2022). General analysis method for global revisit characteristics of satellite constellation with repeating ground tracks. Acta Astronautica.DOI
71. Kuangwei Deng, Weiyong Zhou, Haiyang Li (2022). Experimental device and method design for long-term compression creep of composite solid propellant. International Conference on Advanced Manufacturing Technology and Manufacturing Systems (ICAMTMS).DOI
72. Xiangyue He, Haiyang Li, Jianlei Zhao, Huiru Cui (2022). Configuration design of hybrid constellations with synchronous orbital precession based on rapid coverage analysis. Advances in Space Research.DOI
73. Lin Lu, Haiyang Li, Qibo Peng, Jiyuan Lv (2022). Design and analysis of the transfer trajectory for switching landing site in emergency during the return flight of crewed lunar exploration mission. Acta Astronautica.DOI
74. Kuangwei Deng, Haiyang Li, Jie Xu, Huiru Cui, Zhibin Shen (2022). Long‐Term and Short‐Term Creep Characteristic Analysis for HTPB Propellant. Propellants Explosives Pyrotechnics.DOI
75. Weijing Wu, Haiyang Li, Zhibin Shen, Zijian Fan (2022). Comparative research on tension-compression mechanical properties of the azide propellant. Journal of Physics Conference Series.DOI
76. Qi Wang, Haiyang Li, Lin Lu, Luyi Yang, Shenquan Wang (2022). Global Sensitivity Analysis of Earth-Moon Transfer Orbit Parameters Based on Sobol Method. International Journal of Aerospace Engineering.DOI
77. Weijing Wu, Haiyang Li, Zhibin Shen, Huiru Cui (2022). Research on Constant Speed Tension and Compression Mechanical Properties of Azide Polyether Propellant. Propellants Explosives Pyrotechnics.DOI
78. Lin Lu, Haiyang Li, Wanmeng Zhou, Xinfeng Wu, Huiru Cui (2022). Design and Analysis of Direct Abort Orbits in the Earth-Moon Transfer Phase of Crewed Lunar Exploration Missions. International Journal of Aerospace Engineering.DOI
79. 郭宇，申志彬，李海阳，张漩，卞云龙（2021）. 基于超声振动锯割技术的固体发动机燃烧室解剖方法. 《固体火箭技术》.
80. 陆林，李海阳，周晚萌，刘将辉（2021）. 载人月球极地探测地月转移轨道设计. 《宇航学报》.
81. 郭宇，李海阳，周伟勇，申志彬，丁晓浩（2021）. 基于证据融合的固体发动机贮存寿命评估方法. 《固体火箭技术》.
82. 赵剑，黄悦琛，李海阳，何湘粤（2021）. 垂直起降运载火箭返回轨迹不确定性优化. 《航空学报》.
83. Yu Hua Guo, Zhibin Shen, Haiyang Li, Huiru Cui (2021). Dissection Method of Solid Rocket Motor Chamber Based on Ultrasonic Vibration Sawing. Propellants Explosives Pyrotechnics.DOI
84. Xiangyue He, Haiyang Li (2021). Analytical solutions for Earth discontinuous coverage of satellite constellation with repeating ground tracks. Chinese Journal of Aeronautics.DOI
85. Zhanxin Cui, Haiyang Li, Zhibin Shen, Huiru Cui (2021). Analysis of Load Optimization in Solid Rocket Motor Propellant Grain with Pressure Cure. International Journal of Aerospace Engineering.DOI
86. Zhanxin Cui, Haiyang Li, Zhibin Shen, Huiru Cui (2021). A Viscoelastic Constitutive Model of Propellant with Pressure Cure. Propellants Explosives Pyrotechnics.DOI
87. Jian Cun Zhao, Xiangyue He, Haiyang Li, Lin Lu (2021). An adaptive optimization algorithm based on clustering analysis for return multi-flight-phase of VTVL reusable launch vehicle. Acta Astronautica.DOI
88. Luyi Yang, Haiyang Li, Jin Zhang, Ya-Zhong Luo (2021). Multiphase Trajectory Optimization of a Lunar Return Mission to an LEO Space Station. International Journal of Aerospace Engineering.DOI
89. 陆林，李海阳，刘将辉，杨路易（2020）. 月地应急返回轨道优化设计. 《系统工程与电子技术》.
90. 杨路易，李海阳，张进，周晚萌，陆林（2020）. 基于改进多圆锥截线的月地返回轨道快速设计方法. 《系统工程与电子技术》.
91. Lin Lu, Haiyang Li, Wanmeng Zhou, Jianghui Liu (2020). Design and analysis of a direct transfer trajectory from a near rectilinear halo orbit to a low lunar orbit. Advances in Space Research.DOI
92. Lin Lu, Haiyang Li, Wanmeng Zhou, Jianghui Liu (2020). Three-impulse point return orbit design for the manned lunar high-latitude exploration mission. Acta Astronautica.DOI
93. Xiangyue He, Haiyang Li, Luyi Yang, Jian ping Zhao (2020). Reconfigurable Satellite Constellation Design for Disaster Monitoring Using Physical Programming. International Journal of Aerospace Engineering.DOI
94. Zhangming Zhai, Haiyang Li, Xugang Wang (2020). An adaptive sampling method for Kriging surrogate model with multiple outputs. Engineering With Computers.DOI
95. Jian Cun Zhao, Haiyang Li, Xiangyue He, Yuechen Huang, Jianghui Liu (2020). Uncertainty Analysis for Return Trajectory of Vertical Takeoff and Vertical Landing Reusable Launch Vehicle. Mathematical Problems in Engineering.DOI
96. Luyi Yang, Ya-Zhong Luo, Haiyang Li, Jin Zhang, Zhen Yang, Yuehe Zhu (2020). A Fast Solution to Two-Impulse Lunar Transfer Trajectory based on Machine Learning Method. IEEE Congress on Evolutionary Computation (CEC).DOI
97. Lin Lu, Haiyang Li (2020). Three-Impulse Return Orbit Design and Characteristic Analysis for Manned Lunar Missions. IEEE Access.DOI
98. 申柳雷，李海阳，申志彬（2019）. 基于粘弹性VCFEM的复合固体推进剂等效松弛模量预示方法研究. 《固体火箭技术》.
99. 刘将辉，李海阳（2019）. 对失控翻滚目标逼近的神经网络自适应滑模控制. 《宇航学报》.
100. 刘将辉，李海阳（2019）. 对失控翻滚目标任意位置悬停的模糊控制. 《国防科技大学学报》.
101. 杨路易，李海阳，张进，周晚萌（2019）. 基于多圆锥曲线法的着陆器奔月轨道设计与特性分析. 《宇航学报》.
102. 刘将辉，李海阳，张政，李晓超（2019）. 相对失控翻滚目标悬停的自适应模糊滑模控制. 《航空学报》.
103. 刘将辉，李海阳，陆林，赵剑（2019）. 逼近无控旋转目标航天器的混合势函数安全制导. 《航空学报》.
104. 陆林，杨路易，李海阳，刘将辉（2019）. 载人飞船月地返回轨道优化设计与特性分析. 《系统工程与电子技术》.
105. 刘将辉，李海阳，杨路易，陆林（2019）. 强迫绕飞无控旋转目标的控制策略. 《系统工程与电子技术》.
106. 崔辉如，张斌，申志彬，李海阳（2019）. 考虑粘弹性泊松比的固体推进剂蠕变型本构模型. 《固体火箭技术》.
107. Wanmeng Zhou, Haiyang Li, Hua Wang, Ran Ding (2019). Low-Thrust Trajectory Design Using Finite Fourier Series Approximation of Pseudoequinoctial Elements. International Journal of Aerospace Engineering.DOI
108. Jianghui Liu, Haiyang Li, Ya-Zhong Luo, Jin Zhang (2019). Robust adaptive relative position and attitude integrated control for approaching uncontrolled tumbling spacecraft. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
109. Huiru Cui, Haiyang Li, Zhibin Shen (2019). Cohesive zone model for mode-I fracture with viscoelastic-sensitivity. Engineering Fracture Mechanics.DOI
110. Wanmeng Zhou, Haiyang Li, Bo-yong He, Luyi Yang, Qibo Peng (2019). Fixed-thrust Earth–Moon free return orbit design based on a hybrid multi-conic method of pseudo-perilune parameters. Acta Astronautica.DOI
111. Yuechen Huang, Haiyang Li, Xin Du, Xiangyue He (2019). Mars entry trajectory robust optimization based on evidence under epistemic uncertainty. Acta Astronautica.DOI
112. Jianghui Liu, Haiyang Li, YaKun Zhang, Jian-yong Zhou, Lin Lu, Fuqi Li (2019). Robust Adaptive Relative Position and Attitude Control for Noncooperative Spacecraft Hovering under Coupled Uncertain Dynamics. Mathematical Problems in Engineering.DOI
113. Jianghui Liu, Haiyang Li (2019). Artificial Potential Function Safety and Obstacle Avoidance Guidance for Autonomous Rendezvous and Docking with Noncooperative Target. Mathematical Problems in Engineering.DOI
114. Wanmeng Zhou, Haiyang Li, Feng Huang (2019). Variable Topological Method for Reliability Assessment of Aerospace Vehicle Separation.DOI
115. Huang Yuechen, Li Haiyang, Shen Hongxin (2018). Optimal feedback based control for Mars entry trajectory tracking. Journal Of Systems Engineering And Electronics, Vol. 290, No. 10.DOI
116. 刘将辉，李海阳，张亚坤（2018）. 空间站平均力矩平衡姿态的气动力矩影响. 《国防科技大学学报》.
117. 栗永峰，张赋，申志彬，李海阳（2018）. 固体火箭发动机复合材料壳体裙黏接性能分析. 《国防科技大学学报》.
118. 申柳雷，申志彬，李晶钰，李海阳（2018）. 复合固体推进剂等效力学性能VCFEM细观预示方法. 《国防科技大学学报》.
119. 崔辉如，申志彬，李海阳（2018）. 固体推进剂黏弹性本构模型及其有限元应用研究. 《国防科技大学学报》.
120. 刘将辉，李海阳（2018）. 对失控翻滚目标逼近的增广比例导引律控制. 《系统工程与电子技术》.
121. Huiru Cui, Haiyang Li, Zhi-Bin Shen (2018). Investigation on a novel time-and temperature-dependent cohesive zone model. European Journal of Mechanics - A/Solids.DOI
122. Huiru Cui, Zhibin Shen, Haiyang Li (2018). A novel time dependent cohesive zone model for the debonding interface between solid propellant and insulation. Meccanica.DOI
123. Zhenjiang Sun, Ya-Zhong Luo, Haiyang Li (2018). Uncertainty-Dependent Warning Threshold for Spacecraft Rendezvous Collision Probability. IEEE Transactions on Aerospace and Electronic Systems.DOI
124. Yuechen Huang, Haiyang Li (2018). Reliability-based trajectory optimization using nonintrusive polynomial chaos for Mars entry mission. Advances in Space Research.DOI
125. Huiru Cui, Zhibin Shen, Haiyang Li (2018). A new constitutive equation for solid propellant with the effects of aging and viscoelastic Poisson’s ratio. Meccanica.DOI
126. Liu-Lei Shen, Zhibin Shen, Yan Xie, Haiyang Li (2018). Effective Mechanical Property Estimation of Composite Solid Propellants Based on VCFEM. International Journal of Aerospace Engineering.DOI
127. 贺波勇，李海阳，沈红新，彭祺擘（2017）. 载人登月着陆窗口与定点返回轨道耦合设计. 《国防科技大学学报》.
128. 曹鹏飞，贺波勇，彭祺擘，李海阳（2017）. 载人登月绕月自由返回轨道混合-分层优化设计. 《宇航学报》.
129. 李海阳，贺波勇，曹鹏飞（2017）. 载人登月转移轨道偏差传播分析与中途修正方法概述. 《力学与实践》.
130. 张亚坤，李海阳，李涛（2017）. 遥操作交会对接轨道共享控制策略. 《国防科技大学学报》.
131. 贺波勇，李海阳（2017）. 载人登月着陆器奔月窗口搜索方法. 《航空学报》.
132. Liu-Lei Shen, Zhi-Bin Shen, Haiyang Li, Ze-Yuan Zhang (2017). A Voronoi cell finite element method for estimating effective mechanical properties of composite solid propellants. Journal of Mechanical Science and Technology.DOI
133. Yakun Zhang, Haiyang Li, Ruixue Huang, Jiang-hui Liu (2017). Corrigendum to “Shared control on lunar spacecraft teleoperation rendezvous operations with large time delay” [Acta Astronaut. 137 (2017) 312–319]”. Acta Astronautica.DOI
134. Yuechen Huang, Haiyang Li, Jin Zhang (2017). Uncertainty analysis of reachable set for planetary entry using polynomial chaos. Advances in Space Research.DOI
135. Pengfei Cao, Bo-yong He, Haiyang Li (2017). Analysis of direct transfer trajectories from LL2 halo orbits to LLOs. Astrophysics and Space Science.DOI
136. Wanmeng Zhou, Wang Hua, Fan Zhang, Haiyang Li (2017). Coverage Analysis Tool Design in Object-Oriented Astronautical Simulation Software Using Plugin. International Conference on Information Science and Control Engineering.DOI
137. Yakun Zhang, Ruixue Huang, Haiyang Li, Jiayi Cai (2017). Handling Qualities Evaluation of Time Delay and Predictive Model on Teleoperation Docking. Journal of Spacecraft and Rockets.DOI
138. Zhang Ya-kun, Haiyang Li, Ruixue Huang, Jianghui Liu (2017). Shared control on lunar spacecraft teleoperation rendezvous operations with large time delay. Acta Astronautica.DOI
139. Bo-yong He, Haiyang Li, Jianping Zhou (2017). Solution Domain Analysis of Earth-Moon Quasi-Symmetric Free-Return Orbits. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES.DOI
140. 李海阳（2016）. 固体力学原理. 《国防工业出版社》.
141. 贺波勇，李海阳，周建平（2016）. 载人登月绕月自由返回轨道与窗口精确快速设计. 《宇航学报》.
142. 黄悦琛，李海阳（2016）. 探月返回飞船再入飞行全数字仿真系统设计. 《系统工程与电子技术》.
143. Tao Li, Ruixue Huang, Haiyang Li, Yakun Zhang (2016). Study on navigation and manual steering strategies in the fly-around phase of teleoperation rendezvous and docking. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
144. Zhao Zhao, Jin Zhang, Haiyang Li, Jian-yong Zhou (2016). LEO cooperative multi-spacecraft refueling mission optimization considering J2 perturbation and target’s surplus propellant constraint. Advances in Space Research.DOI
145. Yakun Zhang, Haiyang Li, Ruixue Huang (2016). Investigation into pilot control model base on ANFIS for teleoperation rendezvous and docking. IEEE Advanced Information Management, Communicates, Electronic and Automation Control Conference (IMCEC).DOI
146. Yakun Zhang, Haiyang Li (2016). Handling qualities evaluation of predictive display model for rendezvous and docking in lunar orbit with large time delay.DOI
147. Yuechen Huang, Haiyang Li (2016). Receding Horizon Optimal controller for reference trajectory tracking in Mars entry guidance.DOI
148. Wanmeng Zhou, Hua Wang, Haiyang Li, Guo-Jin Tang (2016). AstroSim: A software framework for aerospace system analysis and simulation.DOI
149. Yakun Zhang, Jianping Zhou, Haiyang Li, Tao Li, Ruixue Huang (2016). Shared Control of Teleoperation Rendezvous and Docking in Lunar Orbit. Journal of Aerospace Engineering.DOI
150. 张亚坤，李海阳（2015）. 级间设计人机联合探月方案. 《国防科技大学学报》.
151. Jin Zhang, Ya-Zhong Luo, Haiyang Li, Guo-Jin Tang (2015). Analysis of multiple asteroids rendezvous optimization using genetic algorithms. IEEE Congress on Evolutionary Computation (CEC).DOI
152. Yuechen Huang, Haiyang Li, Jin Zhang, Xin Du (2015). Mars Atmospheric Entry Guidance Design by Sliding Mode Disturbance Observer-Based Control. Procedia Engineering.DOI
153. Xin Du, Haiyang Li, Yuechen Huang (2015). Efficient Nonlinear Algorithm for Drag Tracking in Entry Guidance. Procedia Engineering.DOI
154. Fuyu Sun, Hua Wang, Guo Shuai, Haiyang Li (2015). SIM - A Flexible, Scalable and Expandable Simulation Platform Applying to Lunar Orbit Rendezvous Mission. International Conference on Simulation and Modeling Methodologies, Technologies and Applications.DOI
155. Wanmeng Zhou, Hua Wang, Fuyu Sun, Haiyang Li (2015). Multi-granularity Modeling of Variable Structured Rocket based on Declarative Language. International Conference on Simulation and Modeling Methodologies, Technologies and Applications.DOI
156. 罗亚中，沈红新，李海阳（2014）. 第五届全国空间轨道设计竞赛总结. 《力学与实践》.
157. 杜昕，李海阳，沈红新（2014）. 基于路径约束分析的跳跃式再入轨迹优化. 《航空学报》.
158. 贺波勇，沈红新，李海阳（2014）. 地月转移轨道设计的改进微分校正方法. 《国防科技大学学报》.
159. 杜昕，李海阳，黄悦琛（2014）. 探月飞船初次再入段纵程的解析预测方法. 《国防科技大学学报》.
160. 张波，李海阳，唐国金（2014）. 环月轨道遥操作交会对接预测共享控制. 《宇航学报》.
161. Hong‐Xin Shen, Lorenzo Casalino, Haiyang Li (2014). Adjoints estimation methods for impulsive Moon-to-Earth trajectories in the restricted three-body problem. Optimal Control Applications and Methods.DOI
162. Bo Zhang, Haiyang Li, Guo-Jin Tang (2014). Human control model in teleoperation rendezvous. Science China Information Sciences.DOI
163. Jin Zhang, Haiyang Li, Ya-Zhong Luo, Guo-Jin Tang (2014). Effects of In-Track Maneuver on the Ground Track of Near-Circular Orbits. Journal of Guidance Control and Dynamics.DOI
164. 沈红新，罗亚中，李海阳（2013）. 第四届全国空间轨道设计竞赛冠军团队解法. 《力学与实践》.
165. Bo Zhang, Guo-Jin Tang, Haiyang Li, Ya-Zhong Luo (2013). Predictive control of teleoperation rendezvous with large time delay. International Conference on Control and Automation.DOI
166. Qibo Peng, Haiyang Li, Hong‐Xin Shen, Guo-Jin Tang (2013). Hybrid Optimization of Powered Descent Trajectory for Manned Lunar Mission. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES.DOI
167. Haiyang Li (2013). Research on the Effects of Time Delay in Teleoperation Rendezvous. Manned Spaceflight.
168. 彭祺擘，李海阳，沈红新，唐国金（2012）. 基于Gauss伪谱法和直接打靶法结合的月球定点着陆轨道优化. 《国防科技大学学报》.
169. 周剑勇，张波，蒋自成，李海阳（2012）. 遥操作交会对接系统研究. 《国防科技大学学报》.
170. 李九人，李海阳，唐国金（2012）. 仅测角导航的自主交会闭环控制偏差分析. 《宇航学报》.
171. Jian-yong Zhou, Jianping Zhou, Jiang Zicheng, Haiyang Li (2012). Investigation into Pilot Handling Qualities in Teleoperation Rendezvous and Docking with Time Delay. Chinese Journal of Aeronautics.DOI
172. Hong‐Xin Shen, Jianping Zhou, Qibo Peng, Haiyang Li (2012). Point return orbit design and characteristics analysis for manned lunar mission. Science China Technological Sciences.DOI
173. Hong‐Xin Shen, Jianping Zhou, Qibo Peng, Haiyang Li, Jiu-tian Li (2012). Multi-objective interplanetary trajectory optimization combining low-thrust propulsion and gravity-assist maneuvers. Science China Technological Sciences.DOI
174. Haiyang Li (2012). Analysis on Manned Lunar Mission Flight Mode. Aerospace Shanghai.
175. Haiyang Li (2012). Rapid Design and Characteristics Analysis of Earth-Moon Transfer Trajectory for Manned Lunar Mission. Manned Spaceflight.
176. Haiyang Li (2012). Simulation Analysis of Reentry Emergency Strategy for Manned Lunar-landing Mission. Manned Spaceflight.
177. Haiyang Li (2012). Researches on teleoperation rendezvous and docking system. Journal of National University of Defense Technology.
178. 沈红新，李海阳，彭祺擘，杜昕（2011）. 探月飞行器定点返回轨迹特性分析. 《国防科技大学学报》.
179. 李九人，李海阳，唐国金（2011）. 对无控旋转目标逼近的自适应滑模控制. 《宇航学报》.
180. Qibo Peng, Hong‐Xin Shen, Haiyang Li (2011). Free return orbit design and characteristics analysis for manned lunar mission. Science China Technological Sciences.DOI
181. Jiuren Li, Haiyang Li, Guo-Jin Tang (2011). Optimal multi-objective trajectory design based on close-looped control for autonomous rendezvous. Science China Technological Sciences.DOI
182. Jin Zhang, Haiyang Li, Ya-Zhong Luo, Guo-Jin Tang (2011). Error analysis for rendezvous phasing orbital control using design of experiments. Aerospace Science and Technology.DOI
183. Jiuren Li, Haiyang Li, Guo-Jin Tang, Ya-Zhong Luo (2011). Research on the strategy of angles-only relative navigation for autonomous rendezvous. Science China Technological Sciences.DOI
184. Hong‐Xin Shen, Jianping Zhou, Qibo Peng, Ya-Zhong Luo, Haiyang Li (2011). Low-thrust trajectory optimization for multiple target bodies tour mission. Theoretical and Applied Mechanics Letters.DOI
185. 沈红新，李海阳，彭祺擘（2010）. 月球返回舱再入制导律设计. 《国防科技大学学报》.
186. 黄海兵，李海阳，王华，唐国金（2010）. 对接组合体初始姿态影响的建模研究. 《国防科技大学学报》.
187. 李桢，李海阳，程文科（2010）. 载人火星任务气动捕获段轨道初步设计. 《国防科技大学学报》.
188. 李桢，周建平，李海阳（2010）. 地球—火星循环轨道研究. 《导弹与航天运载技术(中英文)》.
189. 彭祺擘，李海阳，沈红新（2010）. 基于高斯—伪谱法的月球定点着陆轨道快速优化设计. 《宇航学报》.
190. 李九人，唐国金，李海阳（2010）. 自主交会逼近段的模糊/PID混合控制. 《宇航学报》.
191. 李海阳，李九人，黄海兵（2010）. 空间紧急救援发射点等效构型. 《导弹与航天运载技术(中英文)》.
192. Jin Zhang, Guo-Jin Tang, Ya-Zhong Luo, Haiyang Li (2010). Orbital rendezvous mission planning using mixed integer nonlinear programming. Acta Astronautica.DOI
193. Li-bo Liang, Ya-Zhong Luo, Jin Zhang, Haiyang Li, Guo-Jin Tang (2010). Rendezvous-Phasing Errors Propagation Using Quasi-linearization Method. AIAA Guidance, Navigation, and Control Conference and Exhibit.DOI
194. Ya-Zhong Luo, Zhang Jin, Haiyang Li, Guo-Jin Tang (2010). Space Rendezvous and Docking Mission Planning System Using Object-Oriented Method. AIAA Modeling and Simulation Technologies Conference.DOI
195. Ya-Zhong Luo, Jin Zhang, Haiyang Li, Guo-Jin Tang (2010). Interactive optimization approach for optimal impulsive rendezvous using primer vector and evolutionary algorithms. Acta Astronautica.DOI
196. 周黎妮，李海阳，唐国金（2009）. 空间站基于动量管理的集成能量与姿态控制系统. 《宇航学报》.
197. 李海阳，彭祺擘，周英，唐国金（2009）. 航天器交会对接发射窗口分析. 《宇航学报》.
198. 李海阳，王华，黄海兵，唐国金（2009）. 锥形禁区约束下空间交会的被动安全逼近速度分析. 《宇航学报》.
199. 李九人，李海阳（2009）. 空间紧急救援发射点机动布置研究. 《宇航学报》.
200. 李桢，周建平，程文科，李海阳，彭祺擘（2009）. 环月轨道交会的奔月方案. 《国防科技大学学报》.
201. 彭祺擘，李海阳，李桢，唐国金（2009）. 从空间站出发的奔月轨道设计. 《国防科技大学学报》.
202. 张进，李海阳，罗亚中，唐国金（2009）. 远程导引变轨故障后轨道重构设计与分析. 《国防科技大学学报》.
203. 周黎妮，唐国金，罗亚中，李海阳（2009）. 空间站力矩平衡姿态稳定性研究. 《系统工程与电子技术》.
204. 李九人，李海阳，陈磊，唐国金（2009）. 基于比例导引的空间交会寻的段飞行任务设计. 《飞行力学》.
205. Haiyang Li, Ya-Zhong Luo, Jin-Zhang, Guo-Jin Tang (2009). Optimal multi-objective linearized impulsive rendezvous under uncertainty. Acta Astronautica.DOI
206. Haiyang Li (2009). Obscuration Analysis of Combined Spacecraft Solar Panel. Jisuanji fangzhen.
207. Haiyang Li (2009). Study on Combined Optimal Strategy for Orbit Keeping and Phasing. Aerospace Control and Application.
208. Haiyang Li (2009). An Investigation on Homing Phase Guidance Based on Second-order Nonlinear Equation of Relative Motion. Aerospace Control.
209. Haiyang Li (2009). Optimization of Rendezvous Phasing Strategy with Hybrid Maneuvers. Aerospace Control.
210. 李海阳，杏建军，唐国金，程文科（2008）. 椭圆参考轨道水平圆构形编队设计与演化. 《宇航学报》.
211. 李九人，李海阳，蒋自成（2008）. 空间救援发射窗口分析. 《国防科技大学学报》.
212. 李九人，李海阳，唐国金（2008）. 空间紧急救援关键技术. 《导弹与航天运载技术(中英文)》.
213. 王华，李海阳，唐国金（2008）. 基于碰撞概率的交会对接最优碰撞规避机动. 《宇航学报》.
214. 周黎妮，唐国金，李海阳（2007）. 航天器姿态机动的自抗扰控制器设计. 《系统工程与电子技术》.
215. 王华，唐国金，李海阳（2007）. 基于碰撞概率的交会对接近距离导引段的轨迹安全. 《宇航学报》.
216. 周黎妮，唐国金，罗亚中，李海阳（2007）. 基于稳定度设计的空间站姿态TEA稳定LQR控制器. 《宇航学报》.
217. 王华，李海阳，唐国金（2007）. 视场约束的交会对接V-bar撤离控制研究. 《宇航学报》.
218. 王华，唐国金，李海阳（2007）. 视场约束下V-bar撤离控制的解析计算方法. 《国防科技大学学报》.
219. 王华，李海阳，唐国金（2007）. 交会对接近距离导引段的轨迹安全. 《宇航学报》.
220. Jian-jun Xing, Guo-Jin Tang, Xiaoning Xi, Haiyang Li (2007). Satellite Formation Design and Optimal Stationkeeping Considering Nonlinearity and Eccentricity. Journal of Guidance Control and Dynamics.DOI
221. Ya-Zhong Luo, Guo-Jin Tang, Yongjun Lei, Haiyang Li (2007). Optimization of Multiple-Impulse, Multiple-Revolution, Rendezvous- Phasing Maneuvers. Journal of Guidance Control and Dynamics.DOI
222. Guo-Jin Tang, Ya-Zhong Luo, Haiyang Li (2007). Optimal robust linearized impulsive rendezvous. Aerospace Science and Technology.DOI
223. Haiyang Li (2007). Collision Probability Based Trajectory Safety in Close Range Guidance Phase of Rendezvous and Docking. Journal of Astronautics.
224. 杏建军，李海阳，唐国金，郗晓宁（2006）. 利用数值优化技术设计周期性绕飞的编队轨道. 《国防科技大学学报》.
225. 王华，李海阳，唐国金（2006）. 飞行器碰撞概率计算的一般方法. 《国防科技大学学报》.
226. 袁端才，唐国金，李海阳，蒙上阳（2006）. 基于加速老化与三维粘弹性有限元分析的固体导弹发动机寿命预估. 《兵工学报》.
227. 杏建军，李海阳，唐国金，郗晓宁（2006）. 非线性条件下编队卫星周期性相对运动条件. 《宇航学报》.
228. Ya-Zhong Luo, Haiyang Li, Guo-Jin Tang (2006). Hybrid Approach to Optimize a Rendezvous Phasing Strategy. Journal of Guidance Control and Dynamics.DOI
229. Ya-Zhong Luo, Guo-Jin Tang, Zhong-Gui Wang, Haiyang Li (2006). Optimization of perturbed and constrained fuel-optimal impulsive rendezvous using a hybrid approach. Engineering Optimization.DOI
230. Jian-jun Xing, Guo-Jin Tang, Haiyang Li (2006). New Method of the Analytic Periodic Solution for Spacecraft Formation in Elliptical Orbits. International Astronautical Congress (IAC).DOI
231. Zhou Li-ni, Guo-Jin Tang, Haiyang Li (2006). Feedback Control for Attitude Maneuver Using Matlab/Simulink. International Astronautical Congress (IAC).DOI
232. Ya-Zhong Luo, Guo-Jin Tang, Haiyang Li (2006). Optimization of multiple-impulse minimum-time rendezvous with impulse constraints using a hybrid genetic algorithm. Aerospace Science and Technology.DOI
233. Haiyang Li (2006). Nonlinear and periodic relative motion in spacecraft formations in eccentric orbits. Journal of Tsinghua University(Science and Technology).
234. 吴德隆，李海阳，彭伟斌（2002）. 空间站大型伸展机构的运动稳定性分析. 《宇航学报》.