获奖情况:
北京市自然科学二等奖(1/3)
中国力学学会科技进步二等奖(1/3)
发明专利:
1,龚胜平,苗新元 & 宋雨.基于凸优化的火箭故障后在线重构方法。专利号:CN112395689B.
2,龚胜平,徐梓淇,师鹏 & 程林.一种离散变形模式下变形飞行器的轨迹规划方法. 专利号:CN119200394A.
3,龚胜平,张伟,宋雨 & 苗新元.一种基于凸优化的火箭在线轨迹优化定制化求解器。专利号:CN112001029A.
4,龚胜平,张宗正,程林,李同凯,蔡宇轩,李嘉翔 & 李茗翰,一种小推力轨道转移燃料消耗的快速估计方法。专利号:CN118626798A.
5,龚胜平; 宋雨; 张伟; 苗新元,一种火箭回收仿真平台及实现方法。专利号:CN201911201746.8
代表性论文:
[1] Fu S, Wu D, Shi P, et al. Four-body transit-orbit classification combining lagrangian coherent structures with data mining[J]. Journal of Guidance, Control, and Dynamics, 2025, 48(6): 1314-1333.
[2] Chu Y, Wu D, Li J, et al. Potential of diffractive sail’s sun–earth equilibria for continuous polar observation[J]. Journal of Guidance, Control, and Dynamics, 2024, 47(10): 2204-2212.
[3] Qu C, Cheng L, Gong S, et al. Experience replay enhances excitation condition of neural-network adaptive control learning[J]. Journal of Guidance, Control, and Dynamics, 2025, 48(3): 496-507.
[4] Chu Y, Baoyin H, Gong S. Dynamics and control of sun-facing diffractive solar sails in displaced orbit for asteroid deflection[J]. Aerospace Science and Technology, 2024, 145: 108877.
[5] Song Y, Miao X, Cheng L, et al. The feasibility criterion of fuel-optimal planetary landing using neural networks[J]. Aerospace Science and Technology, 2021, 116: 106860.