李俊峯

1987～1989 北京大學力學系助教、黨委委員、團委書記；

1993～1995 清華大學工程力學系博士後；

1995～1996 清華大學工程力學系講師；

1996～1999 清華大學工程力學系副教授；

1998～1999 在英國Surrey大學參加研製“航天清華1號”衞星，負責姿態控制系統；

1999～2004 清華大學工程力學系教授；

2003～2004 清華大學工程力學系教授、系副主任；

2004～2011 清華大學航天航空學院教授、航空系主任；

2011～2012 清華大學航天航空學院教授、副院長；

2012～2020 清華大學航天航空學院教授、黨委書記；

2019～2020 清華大學副教務長、教務處處長、航天航空學院教授；

2020～至今 清華大學行健書院院長、航天航空學院教授。 ^[2] 

曾任：清華大學教學委員會副主任、教授提名委員會委員；中國空間科學學會常務理事及空間機械委員會副主任、中國力學學會動力學與控制委員會副主任、《力學與實踐》主編、《宇航學報》常務編委，以及《力學學報》、《Theoretical & Applied Mechanics Letters》、《動力學與控制學報》等編委。

現任：清華大學校務委員會委員；中國力學學會常務理事、教育工作委員會主任；中國宇航學會空間控制委員會副主任，中國科學技術協會動力學與控制學科首席科普專家，中國高等教育學會創新創業教育分會副理事長，教育部力學專業教學指導委員會副主任，國務院學位委員會力學學科評議組成員及秘書長；《IEEE Transactions on Aerospace and Electronic Systems》Associate Editor，以及《中國科學》、《深空探測學報》、《空間科學學報》、《空間控制技術與應用》等編委。 ^[2] 

科研方向：航天動力學與控制，涉及航天軌跡優化、深空探測、衞星編隊飛行、充液系統晃動等。

主持科研項目：國家自然科學基金、973及國家重點研發計劃課題等。

主講課程：理論力學、運動穩定性、航天中的奇思妙想（新生研討課）、航天器動力學、飛行器姿態控制系統、高等動力學、現代航天技術概論等。

教學成果：國家級教學名師獎、國家級教學成果一等獎、寶鋼優秀教師特等獎、清華大學新百年教學成就獎，入選國家高層次人才特殊支持計劃（萬人計劃），擔任國家精品課負責人、國家級教學團隊帶頭人，主編《理論力學》（第1、2、3版）被評為“十五”、“十一五”和“十二五”國家級規劃教材，參編《動力學基礎》，翻譯英文著作：《理解航天》（塞勃著）、《航天動力學的數學方法》（巴廷著）、《工程矢量力學》（比爾著）、《靜力學》（希伯勒著）、《動力學》（希伯勒著）。翻譯俄文著作：《力學》（朗道著）、《理論力學》（馬爾契夫著）、《自然@數學》（阿諾德著）、《理論力學習題集》（密歇爾斯基著）等。被清華大學本科生投票評為“清韻燭光·我最喜愛的教師”，被清華大學研究生投票評為“良師益友”。

科研成果：獲得國家科技進步獎、教育部科技進步獎、某科技進步獎、教育部青年教師獎、中國優秀博士後獎等。學術專著有《深空探測動力學與控制》、《太陽帆航天器動力學與控制》、《航天器相對運動軌道動力學》、《細長小行星探測動力學與控制》，在國內外學術期刊發表學術論文約300篇。 ^[2] 

1. 張永隆, 閆翛然, 李俊峯,曾祥遠. 小行星2016 HO3表面動力學環境分析及採樣挑戰. 力學與實踐, 2021, 43(5):6.

2. 武迪, 程林, 王偉, 李俊峯. 基於切換系統的小推力軌跡優化協態初始化方法. 深空探測學報, 2021, 8(5): 528-533

3. 鞏浩然, 武迪, 龔勝平,李俊峯. 用給定轉角分步實現剛體任意有限轉動的研究. 力學與實踐, 2021, 43(3):4.

4. 羅亞中, 李俊峯, 高揚,李九天. 基於"專家型"競賽的航天創新人才培養模式與實踐. 力學與實踐, 2021.

5. 李俊峯. 成長動力學. 力學與實踐，2020，42(2)：242-248

6. 李俊峯. 成長動力學（續）. 力學與實踐，2020，42(6)：811-814

7. 李俊峯, 高永麗, 王曉晶. 制度保障學風傳承 價值引領教研創新——大學教學文化建設與研究. 中國大學教學, 2020(4):83-88

8. 程林，蔣方華，李俊峯. 深度學習在飛行器動力學與控制中的應用研究綜述. 力學與實踐，2020，42(3)：267-276

9. 王秀紅,崔文,李俊峯,何雨帆,李海晶.一種校準編目定軌初始速度的方法. 力學與實踐，2020，42(2)：163-169

10. 藍磊，李俊峯. 柯伊伯帶小行星平運動共振研究. 力學與實踐，2019，41(6)：643-648

11. 劉俊麗，李俊峯.全國周培源大學生力學競賽發展歷程. 力學與實踐，2019，41(3)：357-365

12. 葉志明，李俊峯，王世斌，吳志強，陳立羣，楊驍，武建華，黃毅. 基礎力學課程教材及教學體系分析(一)——國內基礎力學教材基本情況簡述. 力學與實踐，2019，41(3)：314-319

13. 葉志明，李俊峯，王世斌，吳志強，陳立羣，楊驍，武建華，黃毅. 基礎力學課程教材及教學體系分析(二)——國外理論力學教材及教學體系分析. 力學與實踐，2019，41(5)：579-587

14. 葉志明，李俊峯，王世斌，吳志強，陳立羣，楊驍，武建華，黃毅. 基礎力學課程教材及教學體系分析(三)——國外材料力學教材及教學體系分析. 力學與實踐，2019，41(6)：688-698

15. 閆翛然, 李俊峯. YORP效應機理研究與小行星自轉狀態演化仿真. 中國科學：物理學、力學、天文學, 2019, 49(8):12.

16. 張韻, 李俊峯. 小行星的物理性質與結構演化研究進展. 中國科學：物理學、力學、天文學, 2019, 49(8):15.

17. 姜薇, 蔣方華, 李俊峯. 近距離航天器間碰撞概率線性模型的解析修正. 清華大學學報, 2019(9):7.

18. 鄂智博, 李俊峯. 遙感衞星對區域目標可見性的快速計算方法. 清華大學學報, 2019(9):6.

19. 李俊峯. 清華大學錢學森班的理論力學教學實踐. 力學與實踐，2018，40(4)：422-427

20. 陳莉丹, 謝劍鋒, 李俊峯,等. 多目標多約束組合體與飛船軌道維持優化. 宇航學報, 2018, 39(7):8.

21. 劉軍華，李俊峯. 關於剛體角速度的認識與思考. 力學與實踐，2018，40(1)：75-78

22. 姜宇，李俊峯. 小天體平衡點之謎. 力學與實踐，2017，39(5)：509-515

23. 李俊峯，曾祥遠. 不規則小行星引力場內的飛行動力學.力學進展，2017,47(1):429-451

24. 張韻, 劉巖, 李俊峯. 小行星防禦動能撞擊效果評估. 深空探測學報, 2017, 004(001):51-57.

25. 倪彥碩, 施偉璜, 楊洪偉,寶音賀西，李俊峯. 利用Breakwell間距比法制定行星際探測中途修正策略. 深空探測學報, 2016(1):7.

26. 李俊峯，曾祥遠，張韻.小行星的奇特動力學. 力學與實踐，2016，38(6)：603-611

27. 李俊峯. 從動力學角度看力系等效與簡化. 力學與實踐，2016，38(1)：78-79

28. 苗楠，王天舒，李俊峯. 微重環境下液體晃動研究進展. 力學與實踐，2016，38(3)：229-236

29. 苗楠, 李俊峯, 王天舒. 橫向激勵下液體大幅晃動建模分析. 宇航學報, 2016, 37(3):7.

30. 胡天健, 王天舒, 李俊峯,等. 基於互補問題描述單邊接觸的空間機器人動力學建模與數值仿真. 北京大學學報，2016(4):7.

31. 王秀紅, 李俊峯, 高彥平,等. 基於虛擬測距的單星光學監測空間目標定軌方法. 光學精密工程, 2016, 24(7):9.

32. 曾祥遠, 李俊峯, 劉向東. 不規則小天體引力場內的廣義甩擺軌道. 深空探測學報, 2016(1):5.

33. 張韻，李俊峯. 旋轉的沙堡. 力學與實踐，2015，37(4)：549-551

34. 張韻，李俊峯. 碎石堆小行星的散體動力學建模與仿真方法綜述. 力學學報，2015，47(1)：1-7

35. 王雪瑤，龔勝平，李俊峯，彭坤，馬曉兵. 基於快速交會特殊點變軌策略的航天器發射窗口分析. 載人航天, 2015, 21 (6):553-559

36. 曾祥遠, 龔勝平, 李俊峯,等. 應用太陽帆懸停探測啞鈴形小行星. 深空探測學報, 2015, 000(001):48-52.

37. 倪彥碩, 寶音賀西, 李俊峯. 考慮太陽攝動的小行星附近軌道動力學. 深空探測學報, 2014, 1(1):8.

38. 曾祥遠 龔勝平 高雲峯 寶音賀西 李俊峯.非理想太陽帆航天器時間最優交會任務. 清華大學學報，2014 (9)：1240-1244

39. 趙靜，柳寧，吳斌，李俊峯，黃偉芬，趙東明. 中性浮力和失重環境人體運動仿真比較研究. 載人航天, 2014, 20 (6)：517-527

40. 賀晶, 龔勝平, 李俊峯. 利用逃逸能量的太陽帆最快交會軌跡優化. 深空探測學報, 2014, 001(001):60-66.

41. 李俊峯. 提升教學能力，踐行育人使命. 中國大學教學, 2014(9):3.

42. 陳楊，寶音賀西，李俊峯. 考慮功率約束的太陽能電推進軌道優化設計. 清華大學學報，2013，53 (10)：1498-1502

43. 黃岸毅，寶音，李俊峯. 一種組合體航天器帆板的光照遮擋計算新方法. 載人航天, 2013, 19 (5)：1-5

44. 王秀紅, 李俊峯, 王彥榮. 天基照相機監測空間目標定軌方法及精度分析. 光學精密工程, 2013, 021(006):1394-1403.

45. 龔勝平，李俊峯，李京陽. 基於雙體模型下載人登月返回轉移軌道特性分析. 載人航天, 2012, 18 (6)：20-26

46. 陳楊，寶音賀西，李俊峯. 木星探測軌道分析與設計. Acta Astronomica Sinica, 2012, 53 (2):106-118

47. 崔文，寶音賀西，李俊峯. 利用小行星視線矢量的火星探測光學自主導航研究. 力學學報，2012, 44 (6)：1075-1078

48. 曾祥遠 寶音賀西 李俊峯 龔勝平. 太陽帆新型逆向週期軌道. 清華大學學報，2012，52(1)：118-121

49. 李俊峯，崔文，寶音賀西. 深空探測自主導航技術綜述. 力學與實踐，2012, 34 (2)：1-9

50. 馬慶甜 李俊峯 寶音賀西. 橫向連續推力小偏心率人工凍結軌道設計. 空間科學學報，2012, 32 (4)：555-559

1.Liu Chao , Gong Shengping , Li Junfeng. Stability time-scale prediction for main-belt asteroids using neural networks.Monthly notices of the Royal Astronomical Society, 2021, 502 (4):5362-5369

2.E Zhibo , Shi Renhe , Gan Lan , Baoyin Hexi , Li Junfeng. Multi-satellites imaging scheduling using individual reconfiguration based integer coding genetic algorithm.Acta astronautica, 2021, 178: 645-657

3.Wu Di , Wang Wei , Jiang Fanghua , Li Junfeng.Minimum-time low-thrust many-revolution geocentric trajectories with analytical costates initialization. Aerospace science and technology, 2021, 119:107146

4.Wu, Di ; Jiang, Fanghua ; Li, Junfeng.Warm Start for Low-Thrust Trajectory Optimization via Switched System.Journal of guidance, control, and dynamics, 2021, 44 (9):1700-1706

5.Wu Di , Cheng Lin , Jiang Fanghua , Li Junfeng. Rapid generation of low-thrust many-revolution earth-center trajectories based on analytical state-based control. Acta Astronautica, 2021, 187:338-347

6.Zhang Yonglong, Li Junfeng, Zeng Xiangyuan. The dynamical environments analysis of surface particles for different shaped asteroids. ADVANCES IN SPACE RESEARCH, 2021, 67(10):3328-3342.

7.Zhang Yonglong, Li Junfeng, Zeng Xiangyuan, Wen Tongge, Li Ziwen.High-fidelity landing simulation of small body landers: Modeling and mass distribution effects on bouncing motion. AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 119

8.Lin Cheng, Fanghua Jiang, Zhenbo Wang, Junfeng Li. Multi-Constrained Real-Time Entry Guidance Using Deep Neural Networks. IEEE Transactions on Aerospace and Electronic Systems, 2021, 57(1)

9.Gong Haoran , Gong Shengping , Li Junfeng. Pursuit-Evasion Game for Satellites Based on Continuous Thrust Reachable Domain.IEEE transactions on aerospace and electronic systems, 2020, 56 (6):4626-4637

10.Di Wu, Lin Cheng, Junfeng, Li. Warm-Start Multi-Homotopic Optimization for Low-Thrust many-revolution Trajectories. IEEE Transactions on Aerospace and Electronic Systems, 2020,56(6)

11.Liu Chao, Gong Shengping), Li JunFeng. Stability of the coplanar planetary four-body system. RESEARCH IN ASTRONOMY AND ASTROPHYSICS, 2020, 20(9)

12.Sun Hao, Li Junfeng. Analysis on reachable set for spacecraft relative motion under low-thrust. AUTOMATICA 2020, 115

13.Zhemin Chi, Di Wu, Fanghua Jiang, and Junfeng Li. Optimization of Variable-Specific-Impulse Gravity-Assist Trajectories. Journal of Spacecraft and Rockets, 2020, 57(3): 291-299

14.Lin Cheng, Zhenbo Wang, Fanghua Jiang, Junfeng Li. Fast Generation of Optimal Asteroid Landing Trajectories Using Deep Neural Networks. IEEE Transactions on Aerospace and Electronic Systems, 2020,56(4): 2642-2655

15.Lin Cheng, Wang Zhenbo, Jiang Fanghua, Junfeng Li. An Identifier-Actor-Optimizer Policy Learning Architecture for Optimal Control of Continuous-Time Nonlinear Systems. Science China-Physics Mechanics & Astronomy,2020, 63(6)

16.Feng, Ruoyu ; Zhang, Peng ; Li, Junfeng ; Baoyin, Hexi. Kinetic and Dynamic Modeling of Single ActuatorWave-Like Robot. Robotica, 2019, 37 (11):1971-1986

17.Lin Cheng, Zhenbo Wang, Fanghua Jiang, Chengyang Zhou. Real-Time Optimal Control for Spacecraft Orbit Transfer via Multi-Scale Deep Neural Networks. IEEE Transactions on Aerospace and Electronic Systems, 2019, 55(5):2436-2450.

18.Hao Sun, Junfeng Li. Application of Topological Degree Theory to the Equilibrium Point in Irregular Gravitational Field. SIAM Journal on Applied Dynamical Systems, 2019, 18(2): 629-642.

19.Chi Zhemin, Li Haiyang, Jiang Fanghua, Li Junfeng. Power-limited low-thrust trajectory optimization with operation point detection, Astrophysics and Space Science, 2018.5.18, 363(6)

20.Tang Gao, Jiang Fanghua, Li Junfeng. Fuel-optimal low-thrust trajectory optimization using indirect method and successive convex programming, IEEE Transactions on Aerospace and Electronic Systems. 2018, 54 (4):2053-2066

21.Jiang Wei, Li Junfeng, Jiang Fanghua*, and Bernelli-Zazzera Franco. A Simple Method to Design Non-Collision Relative Orbits for Close Spacecraft Formation Flying, Science China Physics, Mechanics & Astronomy, 2018，61（5）

22.Ni Yanshuo, Turitsyn Konstantin, Baoyin Hexi, Li Junfeng. Entropy method of measuring and evaluating periodicity of quasi-periodic trajectories. Science China-Physics Mechanics & Astronomy, 2018, 61(6)

23.Lan, Lei; Wang, Xianyu; Baoyin, Hexi; Li, Junfeng(*), Effect of temporary resonance with heterogeneous Itokawa, Astrophysics and Space Science, 2018, 363(10)

24.Lan Lei, Ni Yanshuo, Jiang Yu, Li Junfeng. Motion of Moonlet in the Binary System 243 Ida. Acta Mechanica Sinica，2018.02, 34(1)：214~224

25.Jiang Yu, Schmidt Juergen, Baoyin Hexi, Li Hengnian, Li Junfeng. Hamiltonian Formulation and Perturbations for Dust Motion around Cometary Nuclei, Earth Moon and Planets, 2017, 120(3): 17-168.

26.Jiang Fanghua, Tang Gao, Li Junfeng. Improving low-thrust trajectory optimization by adjoint estimation with shape-based path, Journal of Guidance, Control and Dynamics, 2017, 40(12): 3280-3287

27.Lan Lei, Wang Xianyu, Baoyin Hexi, Li Junfeng. Bifurcation of Equilibrium Points in the Potential of Heterogeneous Itokawa. Monthly notices of the royal astronomical society, 2017, 470(3): 3417-3426

28.Chi Zhemin，Yang Hongwei，Chen Shiyu，Li Junfeng. Homotopy method for optimization of

variable-specific-impulse low-thrust trajectories，ASTROPHYSICS AND SPACE SCIENCE，2017.11，362(11)

29.Lan Lei，Yang Hongwei，Baoyin Hexi，Li, Junfeng. Retrograde near-circular periodic orbits near

equatorial planes of small irregular bodies，ASTROPHYSICS AND SPACE SCIENCE，2017.9，362(9)

30.Zhang Yun，Richardson Derek C，Barnouin Olivier S，Li Junfeng. Creep stability of the proposed AIDA mission target 65803 Didymos: I. Discrete cohesionless granular physics model. ICARUS, 2017, 294: 98-123

31.Hu Tianjin，Wang Tianshu，Li Junfeng. Gradient Projection of Weighted Jacobian Matrix Method for Inverse Kinematics of a Space Robot With a Controlled-Floating Base. JOURNAL OF DYNAMIC SYSTEMS MEASUREMENT AND CONTROL-TRANSACTIONS OF THE ASME, 2017, 139(5)

32.Hu Tianjian，Zhu Xiaojun，Wang Xueqian, Li Junfeng. Human stochastic closed-loop behavior for master-slave teleoperation using multi-leap-motion sensor. SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 60(3): 374-384

33.Lan Lei，Yang Mo，Baoyin Hexi, Li Junfeng. The periodic dynamics of the irregular heterogeneous celestial bodies. ASTROPHYSICS AND SPACE SCIENCE, 2017, 362(2)

34.Miao Nan，Li Junfeng，Wang Tianshu. Equivalent mechanical model of large-amplitude liquid sloshing under time-dependent lateral excitations in low-gravity conditions. JOURNAL OF SOUND AND VIBRATION, 2017, 386: 421-432

35.Zeng Xiangyuan，Liu Xiangdong，Li Junfeng. Extension of the rotating dipole model with oblateness of both primaries. RESEARCH IN ASTRONOMY AND ASTROPHYSICS, 2017, 17(1)

36.Jiang Yu，Zhang Yun，Baoyin Hexi, Li Junfeng. Dynamical configurations of celestial systems comprised of multiple irregular bodies. ASTROPHYSICS AND SPACE SCIENCE, 2016, 361(9)

37.Hu Tianjian，Wang Tianshu，Li Junfeng. Obstacle Avoidance for Redundant Manipulators Utilizing a Backward Quadratic Search Algorithm. INTERNATIONAL JOURNAL OF ADVANCED ROBOTIC SYSTEMS, 2016, 13

38.Zeng Xiangyuan，Fang Baodong，Li Junfeng. eneralized flyby trajectories around elongated minor celestial bodies as a rotating mass dipole. ACTA MECHANICA SINICA, 2016, 32(3): 535-545

39.Zeng Xiangyuan，Gong Shengping，Li Junfeng. Solar Sail Body-Fixed Hovering over Elongated Asteroids. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2016, 39(6): 1223-1231

40.Wang Tianshu，Miao Nan，Li Junfeng. Large-Amplitude Sloshing Analysis and Equivalent Mechanical Modeling in Spherical Tanks of Spacecraft. JOURNAL OF SPACECRAFT AND ROCKETS, 2016, 53(3): 500-506

41.Wang Xiuhong，Li Junfeng，Du Xinpeng .Orbital correlation of space objects based on orbital elements. RESEARCH IN ASTRONOMY AND ASTROPHYSICS, 2016, 16 ( 3)

42.Hu Tianjian，Gong Shengping，Mu Junshan, Li Junfeng. Switch programming of reflectivity control devices for the coupled dynamics of a solar sail. ADVANCES IN SPACE RESEARCH, 2016, 57(5): 1147-1158

43.Liu Zhuangzhuang，Wang Tianshu，Li Junfeng. Non-intrusive hybrid interval method for uncertain nonlinear systems using derivative information. ACTA MECHANICA SINICA , 2016, 32(1): 170-180

44.Wang Xianyu，Li Junfeng，Gong Shengping. Bifurcation of equilibrium points in the potential field of asteroid 101955 Bennu.MONTHLY NOTICES OF THE ROYAL ASTRONOMICAL SOCIETY, 2016, 455(4): 3724-3734

45.Zeng Xiangyuan，Baoyin Hexi，Li Junfeng. Updated rotating mass dipole with oblateness of one primary (II): out-of-plane equilibria and their stability. ASTROPHYSICS AND SPACE SCIENCE , 2016, 361(1)

46.Zeng Xiangyuan，Baoyin Hexi，Li Junfeng. Updated rotating mass dipole with oblateness of one primary(I): equilibria in the equator and their stability . ASTROPHYSICS AND SPACE SCIENCE , 2016, 361(1)

47.Cai Xingshan, Li Junfeng, Gong Shengping. Solar sailing trajectory optimization with planetary gravity assist. SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 58( 1)

48.Gong Shengping, Li Junfeng. Solar sail periodic orbits in the elliptic restricted three-body problem. CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY , 2015, 121( 2): 121-137

49.Gong Shengping, Li, Junfeng. Equilibria near asteroids for solar sails with reflection control devices.

ASTROPHYSICS AND SPACE SCIENCE, 2015, 355( 2): 213-223

50.Zhang Zhiguo, Gong Shengping, Li Junfeng. Lorentz force time-optimal transfer trajectory design in Jovian magnetic field. ADVANCES IN SPACE RESEARCH , 2015 , 55(4): 1061-1073

51.Zeng Xiangyuan，Jiang Fanghua，Li Junfeng. Study on the connection between the rotating mass dipole and natural elongated bodies. ASTROPHYSICS AND SPACE SCIENCE , 2015, 356(1): 29-42

52.Liu ZhuangZhuang, Wang TianShu, Li JunFeng. A trigonometric interval method for dynamic response analysis of uncertain nonlinear systems. SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 58(4)

53.Zeng Xiangyuan，Jiang Fanghua，Li Junfeng. Asteroid body-fixed hovering using nonideal solar sails. RESEARCH IN ASTRONOMY AND ASTROPHYSICS , 2015 , 15(4): 597-607

54.Gong Shengping，Li Junfeng. Optimal Attitude Maneuver of an Axisymmetric Spinning Solar Sail. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2015 , 51(2): 1462-1474

55.Mu Junshan， Gong Shengping， Li Junfeng. Coupled Control of Reflectivity Modulated Solar Sail for GeoSail Formation Flying. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2015 , 38(4): 740-751

56.Gong Shengping，Li Junfeng. Planetary capture and escape in the planar four-body problem. ASTROPHYSICS AND SPACE SCIENCE, 2015, 357(2)

57.Gong Shengping，Li Junfeng. Analytical criteria of Hill stability in the elliptic restricted three body problem. ASTROPHYSICS AND SPACE SCIENCE, 2015, 358(2)

58.Gong Shengping， Li Junfeng. Asteroid capture using lunar flyby. ADVANCES IN SPACE RESEARCH , 2015, 56(5): 848-858

59.Gong Shengping，Li Junfeng，Jiang Fanghua. Interplanetary trajectory design for a hybrid propulsion system. AEROSPACE SCIENCE AND TECHNOLOGY , 2015, 45: 104-113

60.Gong Shengping，Li Junfeng. A New Inclination Cranking Method for a Flexible Spinning Solar Sail. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2015, 51(4): 2680-2696

61.Mu Junshan，Gong Shengping，Ma Pengbin, Li JunFeng. Dynamics and control of flexible spinning solar sails under reflectivity modulation. ADVANCES IN SPACE RESEARCH, 2015, 56(8): 1737-1751

62.Tang Gao，Jiang FangHua，Li JunFeng. Low-thrust trajectory optimization of asteroid sample return mission with multiple revolutions and moon gravity assists. SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 58(11)

63.Zhang Yun，Baoyin Hexi，Li Junfeng. Effects of orbital ellipticity on collisional disruptions of rubble-pile asteroids. ASTROPHYSICS AND SPACE SCIENCE, 2015, 360(1)

64.Wu Zhigang，Jiang Fanghua，Li Junfeng. Extension of frozen orbits and Sun-synchronous orbits around terrestrial planets using continuous low-thrust propulsion. ASTROPHYSICS AND SPACE SCIENCE, 2015, 360(1)

65.Mu Junshan, Gong Shengping, Li Junfeng. Coupled Control of Reflectivity Modulated Solar Sail for GeoSail Formation Flying, Journal of Guidance, Control, and Dynamics, 2014, 37(1):1-12

66.Zeng Xiangyuan, Gong Shengping, Li Junfeng. Fast solar sail rendezvous mission to near Earth asteroids. Acta Astronautica, 2014, 105:40-56.

67.Cai Xingshan, Chen Yang, Li Junfeng. Low-thrust trajectory optimization in a full ephemeris model. Acta Mechanica Sinica, 2014, 30(5):615-627

68.He Jing, Gong Shengping, Jiang Fanghua, Li Junfeng. Time-optimal rendezvous transfer trajectory for restricted cone-angle range solar sails. Acta Mechanica Sinica,2014, 30(5):628-635

69.Zeng Xiangyuan, Gong Shengping, Li Junfeng.Earth-crossing asteroid intercept mission with a solar sail spacecraft. IEEE Aerospace and Electronic Systems Magazine, 2014, 29(10): 4-15

70.Gong Shengping, Li Junfeng. Solar sail heliocentric elliptic displaced orbits. Journal of Guidance, Control, and Dynamics, 2014, 37(6): 2021-2025.

71.Zhang Zhiguo,Gong Shengping, Li Junfeng. Lorentz force time-optimal transfer trajectory design in Jovian magnetic field. Advances in Space Research, 2014

72.Zhang Zhiguo,Gong Shengping, Li Junfeng. The fuel-optimal trajectory for finite-thrust LUNAR ASCENT. Aerospace Science and Technology, 2014,39(12): 675-684.

73.Gong Shengping, Li Junfeng. Solar Sail Halo Orbit Control using Reflectivity Control Devices. Transactions of the Japan Society for Aeronautical and Space Sciences, 2014, 57(5): 279-288.

74.Hu Xiaosai, Gong Shengping, Li Junfeng. Attitude stability criteria of axisymmetric solar sail. Advance in Space Research，2014，54(1): 72-81.

75.Gong Shengping, Li Junfeng, Simo Jules. Orbital Motions of a Solar Sail Around the L2 Earth-Moon Libration Point. Journal of Guidance Control and Dynamics, 2014, 37(4): 1349+-

76.Gong Shengping, Li Junfeng. Fuel consumption for interplanetary missions of solar sailing. Science China Physics, Mechanics & Astronomy,2014,57(3): 521-531.

77.Zhang Peng, Li Junfeng, Gong Shengping. Fuel-optimal trajectory design using solar electric propulsion under power constraints and performance degradation. Science China Physics, Mechanics & Astronomy,2014,57(6): 1090-1097.

78.Wang Xianyu,Gong Shengping, Junfeng Li. A method for classifying orbits near asteroids. Acta Mechanica Sinica,2014, 30(3): 316-325.

79.Hexi Baoyin, Junfeng Li. A survey on orbital dynamics and navigation of asteroid missions. Acta Mechanica Sinica,2014, 30(3): 282-293.

80.Chen Yang, Baoyin Hexi, Li Junfeng. Accessibility of Main-Belt Asteroids via Gravity Assists. Journal of Guidance, Control and Dynamics. 2014,37(2): 623-632

81.Gong Shengping, Li Junfeng. Spin-stabilized solar sail for displaced solar orbits. Aerospace Science and Technology, 2014, 32(1):188-199

82.Jiang Yu, Baoyin Hexi, Li Junfeng, Li Hengnian. Orbits and manifolds near the equilibrium points around a rotating asteroid. Astrophysics and Space Science,2014, 349(1): 83-106

83.Ma Xue, Li Junfeng. Artificial frozen orbits around Mercury. Astrophysics and Space Science,2013, 348(2): 345-365

84.Ma Xue, Li Junfeng. Distant quasi-periodic orbits around Mercury. Astrophysics and Space Science, 2013, 343(1): 83-93.

85.Guo Tieding, Li Junfeng, Baoyin Hexi, Jiang Fanghua. Pseudospectral methods for trajectory optimization with interior point constraints: Verification and applications. IEEE Transactions on Aerospace and Electronic Systems, 2013,49(3):2005-2017

86.Jin Jin, Baoyin Hexi, Li Junfeng.Attitude scheme for satellite with defective inertia characteristic. Aircraft Engineering and Aerospace Technology, 2013,85(5):422-431

87.Mu Junshan, Gong Shengping, Li Junfeng. Reflectivity-controlled solar sail formation flying for magnetosphere mission. Aerospace Science and Technology, 2013, 30(1):339-348

88.Baoyin Hexi, Yu Yang, Li Junfeng. Orbital maneuver for a rotating tethered system via tidal forces. Journal of Spacecraft and Rockets, 2013, 50(5):1060-1068

89.Ma Xue, Li Junfeng, Baoyin Hexi, et al. Distant orbits around Mercury. Advances in the Astronautical Sciences, 2012, 145: 231-239

90.He Jing, Gong Shengping, Li Junfeng. A curved surface solar radiation pressure force model for solar sail deformation. Science China Physics, Mechanics & Astronomy,2012,55(1): 141-155

91.Gong Shengping, Li Junfeng, Baoyin Hexi. A new solar sail orbit. Science China Technological Sciences,2012,55(3): 848-855

92.Li Zhengxue, Li Junfeng, Baoyin Hexi. Sensitivity analysis for a type of statically stable sailcrafts. Acta Mechanica Sinica,2012, 28(2): 532-542

93.Qi Feng, Bi Laiye, Wang Tianshu, Li Junfeng. The experimental study on the contact process of passive walking. Acta Mechanica Sinica,2012, 28(4): 1163-1168

94.Jiang Fanghua, Baoyin Hexi, Li Junfeng. Practical Techniques for Low-Thrust Trajectory Optimization with Homotopic Approach. Journal of Guidance Control and Dynamics, 2012, 35(1): 245-258

95.Guo Tieding, Jiang Fanghua, Li Junfeng. Homotopic approach and pseudospectral method applied jointly to low thrust trajectory optimization. Acta Astronautica, 2012, 71 (1-2): 38-50 ^[2]