一、关于运动稳定性 1.Li Junfeng, On the stability of dissipative mechanical systems with circulatory forces. ZAMP, 1997, 48(1):161-164. 2.Li Junfeng, Li Xiaotian, Wang Zhaolin, New theorems on stability of mechanical systems with circulatory forces,ZAMP ,1999,50(8):839-843 3.Li Junfeng, Wang Zhaolin, Stability of Nonlinear Vibrations of a Deploying Flexible Beam of a Spacecraft, ZAMP,1999,50(10):999-1005 4.Li Junfeng, Wang Zhaolin, Stability of non-conservative linear gyroscopic systems. Applied Mathematics and Mechanics, 1996,17(12): 1171-1176 5.李俊峰,王照林,约束阻尼系统的稳定性研究, 清华大学学报, 1998, 38(11):84-86 二、关于卫星编队飞行 1. Li Junfeng, Meng Xin, Gao Yunfeng,Li Xiang, Study on relative orbital configuration in satellite formation flying, Acta Mechanica Sinca, 2005, 21(1):87-94 2. Meng Xin, Li Junfeng, Gao Yunfeng, A Useful Relative Motion Description Method for Perturbations Analysis in Satellite Formation Flying, Applied Mathematics and Mechanics, 2005, 26(11):1464-1474 3. H.Baoyin, Li Junfeng, Gao Yunfeng, Dynamical behaviors and relative trajectories of the spacecraft formation flying, Aerospace Science and Technology, 2002,4(6):295-301 4. Gao Yunfneg, Baoyinhexi, Li Junfeng, Comparison of two methods in satellite formation flying, Applied Mathematics and Mechanics, 2003, 24(8):799-804 5. Humei Wang, Wei Yang, Junfeng Li, Solution set on the natural satellite formation orbits under first-order earth’s non-spherical perturbation, Acta Mechanica Sinica,2005,21(5):503-510 6.李俊峰,孟鑫,高云峰,李响,卫星编队飞行相对轨道最小摄动条件研究,清华大学学报,2004,44(2):224-227... 一、关于运动稳定性 1.Li Junfeng, On the stability of dissipative mechanical systems with circulatory forces. ZAMP, 1997, 48(1):161-164. 2.Li Junfeng, Li Xiaotian, Wang Zhaolin, New theorems on stability of mechanical systems with circulatory forces,ZAMP ,1999,50(8):839-843 3.Li Junfeng, Wang Zhaolin, Stability of Nonlinear Vibrations of a Deploying Flexible Beam of a Spacecraft, ZAMP,1999,50(10):999-1005 4.Li Junfeng, Wang Zhaolin, Stability of non-conservative linear gyroscopic systems. Applied Mathematics and Mechanics, 1996,17(12): 1171-1176 5.李俊峰,王照林,约束阻尼系统的稳定性研究, 清华大学学报, 1998, 38(11):84-86 二、关于卫星编队飞行 1. Li Junfeng, Meng Xin, Gao Yunfeng,Li Xiang, Study on relative orbital configuration in satellite formation flying, Acta Mechanica Sinca, 2005, 21(1):87-94 2. Meng Xin, Li Junfeng, Gao Yunfeng, A Useful Relative Motion Description Method for Perturbations Analysis in Satellite Formation Flying, Applied Mathematics and Mechanics, 2005, 26(11):1464-1474 3. H.Baoyin, Li Junfeng, Gao Yunfeng, Dynamical behaviors and relative trajectories of the spacecraft formation flying, Aerospace Science and Technology, 2002,4(6):295-301 4. Gao Yunfneg, Baoyinhexi, Li Junfeng, Comparison of two methods in satellite formation flying, Applied Mathematics and Mechanics, 2003, 24(8):799-804 5. Humei Wang, Wei Yang, Junfeng Li, Solution set on the natural satellite formation orbits under first-order earth’s non-spherical perturbation, Acta Mechanica Sinica,2005,21(5):503-510 6.李俊峰,孟鑫,高云峰,李响,卫星编队飞行相对轨道最小摄动条件研究,清华大学学报,2004,44(2):224-227 7.孟鑫,李俊峰,编队飞行卫星相对运动的零J2摄动条件研究,清华大学学报,2004,44(2):219-223 8.孟鑫,李俊峰,高云峰,卫星编队飞行相对轨道的摄动研究,宇航学报,2004,25(4):473-478 9. 李响,李俊峰,高云峰. 卫星编队飞行中相对轨道构形研究,清华大学学报,2002,42(11):1496-1499 10. 苏罗鹏,李俊峰,高云峰,卫星编队飞行相对姿态控制,清华大学学报,2003,43(5):683-685 三、充液航天器晃动动力学 1. H.Baoyin, Li Junfeng, Gao Yunfeng, Wang Zhaolin, Damping computation of sloshing liquid in the containers of spacecraft, Acta Mechanica Sinica,2003,19(2):189-192 2.李俊峰,鲁异,宝音贺西,王为,贮箱内液体小幅晃动的频率和阻尼计算,工程力学,2005,22(6):87-90 3.陈科,李俊峰,王天舒,矩形贮箱内液体非线性晃动动力学建模与分析,力学学报,2005,37(3):339-345 4.周宏,李俊峰,王天舒,低重环境航天器贮箱内三维液体晃动数值模拟,清华大学学报,2005,45(5):658-661 |