职称:教授

E-mail address:jiangfh@tsinghua.edu.cn

个人简介

蒋方华,男,1982年生,湖南永州人,清华大学航天航空学院长聘教授、博士生导师,国家优秀青年基金获得者。从2000年9月起,一直在清华大学航天航空学院学习和工作,研究方向为航天动力学与控制,讲授“理论力学”、“航天动力学”等课程。在航天动力学优化领域取得创新成果,发表SCI期刊论文60余篇,研究成果被国内外知名学者广泛好评和采用,2022-2024年连续入选Stanford/Elsevier前2%科学家榜单,在我国载人航天工程、遥感卫星工程、电推卫星工程应用中做出重要贡献。带领学生获得国际空间探测轨迹优化大赛1冠军2亚军1季军,并举办一届大赛。主持国家自然科学基金青年项目、面上项目、重点项目课题、联合项目课题、优青项目,国家重点研发计划项目子课题,863项目课题,航天院所委托项目等多项,获省部级科技一等奖2项和中国力学学会自然科学一等奖1项。任SCI期刊《Aerospace》副主编、中科院一区期刊《Astrodynamics》创刊编委,美国航空航天学会终身高级会员、中国力学学会会员、中国宇航学会会员。

通讯地址:清华大学蒙民伟科技大楼N931室,100084

邮箱: jiangfh@tsinghua.edu.cn

教育背景

2007.9~2009.7 清华大学航天航空学院 力学 博士研究生(硕转博)

2004.9~2007.7 清华大学航天航空学院 力学 硕士研究生

2000.9~2004.7 清华大学工程力学系 工程力学 本科生

工作履历

2025.6~至今 清华大学航天航空学院 长聘教授

2022.8~2025.6 清华大学航天航空学院 长聘副教授

2016.6~2022.8 清华大学航天航空学院 准聘副教授

2014.12~2016.6 清华大学航天航空学院 副教授

2011. 6~2014.12 清华大学航天航空学院 助理研究员

2009. 7~2011.6 清华大学航天航空学院 博士后

学术兼职

2024.11~至今 《Aerospace》(SCI) 副主编

2021.2~2024.11 《Aerospace》(SCI) 编委

2021.1~至今 《动力学与控制学报》 青年编委

2016.1~至今 《Astrodynamics》(ESCI) 创刊副主编

2015.12~至今 美国航空航天学会 终身高级会员

2018.10~2021.10 《清华大学学报(自然科学版)》(EI) 特约编委

研究领域

航天器轨道动力学与控制、空间探测任务轨道设计与轨迹优化、卫星在轨任务规划。

研究概况

主要从事航天动力学与控制研究,结合国家重大航天工程需求与学科发展前沿,解决轨道动力学优化控制难题。航天是一项高投入、高风险、高回报的事业,因此需要尽力优化航天器的飞行轨道,以便减少投入、提高回报,并且满足工程约束、降低风险。对电推进小推力航天器轨迹优化问题,建立了解析法结合神经网络的轨迹同伦优化理论与高效率计算方法,实现了精准快速优化求解。对多天体引力耦合场中的航天器低能轨道设计与控制问题,开发了力模型自适应同伦延拓轨道设计方法,发现了诸多新型转移轨道。对深空多小行星探测、近地大规模星群在轨维护、空间碎片云清除等多目标探测轨道全局优化问题,提出了融合数据驱动与智能搜索的全局分层优化方法,在国际大赛中摘金夺银。

奖励与荣誉

2025年,第十一届中国力学学会自然科学奖一等奖

2025年,第六届全国高校航空航天类专业本科毕业设计成果交流会一等奖指导教师

2024年,清华大学优秀博士学位论文指导教师

2023年,中国力学学会授予“CTOC突出贡献个人”(CTOC:中国空间轨道设计竞赛)

2023年,第四届全国高校航空航天类专业本科毕业设计成果交流会特等奖指导教师

2023年,清华大学大学生研究训练(SRT)计划优秀指导教师特等奖

2022年,清华大学2021年度教学优秀奖

2021年,第11届国际空间探测轨迹优化大赛冠军

2021年,第二届全国航空航天类专业本科毕设成果交流会特等奖指导教师

2021年,北京市普通高校优秀本科毕业设计论文优秀指导教师

2020年,国家自然科学基金优秀青年科学基金资助

2019年,第10届国际空间探测轨迹优化大赛亚军

2019年,上海市技术发明奖一等奖

2017年,军队科学技术进步奖一等奖

2015年,第8届国际空间探测轨迹优化大赛亚军

2010年,第5届国际空间探测轨迹优化大赛季军

2010年,第2届中国空间轨道设计竞赛冠军

2009年,清华大学优秀博士学位论文和优秀博士毕业生

学术成果

发表中英文论文、论著如下:

Liu ZH, Jiang Fanghua. Design of two-impulse soft-landing trajectories from unstable periodic orbits around an irregular asteroid by gravity model continuation[J]. IEEE Transactions on Aerospace and Electronic Systems, 2025, 61(2): 5402-5415.

Xie X, Jiang Fanghua, Li JF. Insertion error correction and configuration maintenance optimization for geocentric gravitational wave detectors[J]. Acta Astronautica, 2025, 231: 15-24.

Zhang Z, Zhang N, Guo X, Wu D, Xie X, Yang J, Jiang Fanghua, Baoyin HX. Sustainable Asteroid Mining: On the design of GTOC12 problem and summary of results[J]. Astrodynamics, 2025, 9(1): 3-17.

郭祥, 武迪, 蒋方华. 燃料最优小推力轨迹平滑化求解方法的平滑参数上限分析[J]. 中国科学: 物理学 力学 天文学, 2025, 55(2): 224506.

江星宇, 薛锋丰, 蒋方华, 师鹏, 龚胜平. 刚弹耦合运载火箭自适应改进PD控制器[J]. 北京航空航天大学学报, 2024, online.

Xie X, Jiang Fanghua, Li JF. Low frequency hierarchical cooperative impulse control for gravitational wave detector formation keeping[J]. Journal of Guidance Control and Dynamics, 2024, 47(6): 1167-1181.

Zhang Z, Zhang N, Chen ZR, Jiang Fanghua, Baoyin HX, Li JF. Global trajectory optimization of multispacecraft successive rendezvous using multitree search[J]. Journal of Guidance Control and Dynamics, 2024, 47(3): 503-517.

Li Z, Wu D, Li HN, Jiang Fanghua. Minimum-time low-thrust geocentric transfer with longitude estimation and costate prediction[J]. Journal of Guidance Control and Dynamics, 2024, 47(1): 175-186.

Guo X, Wu D, Jiang Fanghua. Multiphase homotopic approaches for best solution to low-thrust geocentric trajectories[J]. IEEE Transactions on Aerospace and Electronic Systems, 2024, 60(4): 3979-3992.

Ÿ武迪, 郭祥, 蒋方华, 宝音贺西, 李俊峰. 连续小推力轨迹优化间接法研究进展综述[J]. 宇航学报, 2024, 45(7): 995-1007.

Guo X, Wu D, Jiang Fanghua. Costate scaling method for Mayer-form multirendezvous trajectory optimization problem[J]. Journal of Spacecraft and Rockets, 2024, 61(3): 878-888.

Li Z, Li HN, Jiang Fanghua, Li JF. Perturbed low-thrust geostationary orbit transfer guidance via polynomial costate estimation[J]. Chinese Journal of Aeronautics, 2024, 37(3): 181-193.

Zhang TX, Wu D, Jiang Fanghua, Li JF. A pseudoequinoctial shaping method with Fourier approximation for low-thrust trajectory optimization[J]. Advances in Space Research, 2024, 73(1): 126-142.

Wang ZW, Jiang Fanghua. Analytical optimal solution for the reachable domain of low-thrust spacecraft[J]. Journal of Spacecraft and Rockets, 2024, 61(1): 274-284.

Guo X, Wu D, Jiang Fanghua. Minimum-time rendezvous via simplified initial costate normalization and auxiliary orbital transfer[J]. Journal of Guidance Control and Dynamics, 2023, 46(8): 1627-1636.

Li Z, Li HN, Zhou H, Jiang Fanghua. Learning-based polynomial approximation of minimum-time low-thrust transfers to geostationary orbit[J]. IEEE Transactions on Aerospace and Electronic Systems, 2023, 59(3): 2388-2401.

Zhang Z, Zhang N, Guo X, Wu D, Xie X, Li JY, Yang J, Chen SY, Jiang Fanghua, Baoyin HX, Li HY, Zheng HX, Duan XW. GTOC 11: Results from Tsinghua University and Shanghai Institute of Satellite Engineering[J]. Acta Astronautica, 2023, 202: 819-828.

Yang J, Zhang Z, Jiang Fanghua, Li JF. Low-energy transfer design of heliocentric formation using lunar swingby on the example of LISA[J]. Aerospace, 2023, 10(1): 18.

Xie X, Jiang Fanghua, Li JF. Design and optimization of stable initial heliocentric formation on the example of LISA[J]. Advances in Space Research, 2023, 71(1): 420-438.

Wu D, Guo X, Jiang Fanghua, BaoyinHX. Atlas of optimal low-thrust rephasing solutions in circular orbit[J]. Journal of Guidance Control and Dynamics, 2023, 46(5): 856-870.

Wang ZW, Cheng L, Jiang Fanghua. Approximations for secular variation maxima of classical orbital elements under low thrust[J]. Mathematics, 2023, 11(3): 744.

Guo X, Ren D, Wu D, Jiang Fanghua. DNN estimation of low-thrust transfer time: Focusing on fast transfers in multi-asteroid rendezvous missions[J]. Acta Astronautica, 2023, 204: 518-530.

Zhang HJ, Ren D, Jiang Fanghua. A beam search-based channel allocation method for interference mitigation of NGSO satellites with multi-beam antennas[J]. Aerospace, 2022, 9(4): 177.

Wu D, Zhang TX, Zhong Y, Jiang Fanghua, Li JF. Analytical shaping method for low-thrust rendezvous trajectory using cubic spline functions[J]. Acta Astronautica, 2022, 193: 511-520.

Wu D, Cheng L, Jiang Fanghua, Li JF. Analytical costate estimation by a reference trajectory-based least-squares method[J]. Journal of Guidance Control and Dynamics, 2022, 45(8): 1529-1537.

Li QQ, Tao YM, Jiang Fanghua. Orbital stability and invariant manifolds on distant retrograde orbits around Ganymede and nearby higher-period orbits[J]. Aerospace, 2022, 9(8): 454.

Zhang TX, Wu D, Jiang Fanghua, Zhou H. A new 3D shaping method for low-thrust trajectories between non-intersect orbits[J]. Aerospace, 2021, 8(11): 315.

Wu D, Wang W, Jiang Fanghua, Li JF. Minimum-time low-thrust many-revolution geocentric trajectories with analytical costates initialization[J]. Aerospace Science and Technology, 2021, 119: 107146.

Wu D, Jiang Fanghua, Li JF. Warm start for low-thrust trajectory optimization via switched system[J]. Journal of Guidance Control and Dynamics, 2021, 44 (9): 1700-1706.

Wu D, Cheng L, Jiang Fanghua, Li JF. Rapid generation of low-thrust many-revolution earth-center trajectories based on analytical state-based control[J]. Acta Astronautica, 2021, 187: 338-347.

Cheng L, Wang ZB, Jiang Fanghua, Li JF. Adaptive neural network control of nonlinear systems with unknown dynamics[J]. Advances in Space Research, 2021, 67(3): 1114-1123.

Cheng L, Jiang Fanghua, Wang ZB, Li JF. Multiconstrained real-time entry guidance using deep neural networks[J]. IEEE Transactions on Aerospace and Electronic Systems, 2021, 57(1): 325-340.

Chen SY, Jiang Fanghua, Li HY, Baoyin HX. Optimization for multitarget, multispacecraft impulsive rendezvous considering J2 perturbation[J]. Journal of Guidance Control and Dynamics, 2021, 44(10): 1811-1822.

武迪, 闫翛然, 李海洋, 蒋方华. 火星探测器接近段器地组合导航方法[J]. 中国科学:技术科学, 2020, 50(9): 1150-1159.

迟哲敏, 李俊峰, 蒋方华, 宝音贺西. 变比冲连续小推力轨迹优化方法综述[J]. 飞控与探测, 2020, 3(4): 58-67.

程林, 蒋方华, 李俊峰. 深度学习在飞行器动力学与控制中的应用研究综述[J]. 力学与实践, 2020, 42(3): 267-276.

Meng YZ, Li HN, Jiang Fanghua. Polynomial-based method for determining coast-terminating zero of fuel-optimal time-fixed trajectory[J]. Astrophysics and Space Science, 2020, 365(1): 8.

Chi ZM, Wu D, Jiang Fanghua, Li JF. Optimization of variable-specific-impulse gravity-assist trajectories[J]. Journal of Spacecraft and Rockets, 2020, 57(2): 291-299.

Chi ZM, Jiang Fanghua, Tang G. Optimization of variable-specific-impulse gravity-assist trajectories via optimality-preserving transformation[J]. Aerospace Science and Technology, 2020, 101: 105828.

Cheng L, Wang ZB, Song Y, Jiang Fanghua. Real-time optimal control for irregular asteroid landings using deep neural networks[J]. Acta Astronautica, 2020, 170: 66-79.

Cheng L, Wang ZB, Jiang Fanghua, Li JF. Fast generation of optimal asteroid landing trajectories using deep neural networks[J]. IEEE Transactions on Aerospace and Electronic Systems, 2020, 56(4): 2642-2655.

Cheng L, Wang ZB, Jiang Fanghua, Li JF. An identifier-actor-optimizer policy learning architecture for optimal control of continuous-time nonlinear systems[J]. Science China-Physics Mechanics & Astronomy, 2020, 63(6): 264511.

Cheng L, Li HN, Wang ZW, Jiang Fanghua. Fast solution continuation of time-optimal asteroid landing trajectories using deep neural networks[J]. Acta Astronautica, 2020, 167: 63-72.

于龙江, 蒋方华, 姜洋, 喜进军. 敏捷卫星一般轨迹主动推扫成像模式设计[J]. 航天器工程, 2019, 28(1): 27-34.

姜薇, 蒋方华, 李俊峰. 近距离航天器间碰撞概率线性模型的解析修正[J]. 清华大学学报(自然科学版), 2019, 59(9): 705-711.

程林, 张庆振, 蒋方华. 基于在线模型辨识的飞行器多约束复合制导技术[J]. 清华大学学报(自然科学版), 2019, 59(9): 712-719.

Cheng L, Wang ZB, Jiang Fanghua. Real-time control for fuel-optimal Moon landing based on an interactive deep reinforcement learning algorithm[J]. Astrodynamics, 2019, 3(4): 375-386.

Cheng L, Wang ZB, Jiang Fanghua, Zhou CY. Real-time optimal control for spacecraft orbit transfer via multiscale deep neural networks[J]. IEEE Transactions on Aerospace and Electronic Systems, 2019, 55(5): 2436-2450.

Yang HW, Tang G, Jiang Fanghua. Optimization of observing sequence based on nominal trajectories of symmetric observing configuration[J]. Astrodynamics, 2018, 2(1): 25-37.

倪彦硕, 蒋方华, 李俊峰. 航天动力学的数学方法[M]. 北京: 中国宇航出版社, 2018.

Wu D, Song Y, Chi ZM, E ZB, Sun H, Baoyin HX, Jiang Fanghua. Problem A of the 9th China trajectory optimization competition: Results found at Tsinghua University[J]. Acta Astronautica, 2018, 150: 204-212.

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

Li HY, Li JY, Jiang Fanghua. Dynamics and control for contactless interaction between spacecraft and tumbling debris[J]. Advances in Space Research, 2018, 61(1): 154-166.

Jiang W, Li JF, Jiang Fanghua, Bernelli-Zazzera F. A simple method to design non-collision relative orbits for close spacecraft formation flying[J]. Science China-Physics Mechanics & Astronomy, 2018, 61(5): 054511.

Chi ZM, Li HY, Jiang Fanghua, Li JF. Power-limited low-thrust trajectory optimization with operation point detection[J]. Astrophysics and Space Science, 2018, 363(6): 122.

李舒航, 蒋方华. 悬挂点匀速转动时摆锤圆周运动的存在性与稳定性分析[J]. 应用数学和力学, 2018, 39(2): 183-198.

Ma PB, Wang TS, Jiang Fanghua, Mu JS, Baoyin HX. Autonomous navigation of Mars probes by single X-ray pulsar measurement and optical data of viewing Martian moons[J]. Journal of Navigation, 2017, 70(1): 18-32.

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

Tang G, Jiang Fanghua. Capture of near-Earth objects with low-thrust propulsion and invariant manifolds[J]. Astrophysics and Space Science, 2016, 361(1): 10.

Jiang Fanghua, Tang G. Systematic low-thrust trajectory optimization for a multi-rendezvous mission using adjoint scaling[J]. Astrophysics and Space Science, 2016, 361(4): 117.

余婧, 喜进军, 于龙江, 蒋方华. 敏捷卫星同轨多条带拼幅成像模式研究[J]. 航天器工程, 2015(2): 27-34.

曾祥远, 龚胜平, 李俊峰, 蒋方华, 宝音贺西. 应用太阳帆悬停探测哑铃形小行星[J]. 深空探测学报, 2015, 2(1): 48-52.

Zeng XY, Jiang Fanghua, Li JF, Baoyin HX. Study on the connection between the rotating mass dipole and natural elongated bodies[J]. Astrophysics and Space Science, 2015, 356(1): 29-42.

Zeng XY, Jiang Fanghua, Li JF. Asteroid body-fixed hovering using nonideal solar sails[J]. Research in Astronomy and Astrophysics, 2015, 15(4): 597-607.

Wu ZG, Jiang Fanghua, Li JF. Extension of frozen orbits and Sun-synchronous orbits around terrestrial planets using continuous low-thrust propulsion[J]. Astrophysics and Space Science, 2015, 360(1): 12.

Tang G, Jiang Fanghua, Li JF. Low-thrust trajectory optimization of asteroid sample return mission with multiple revolutions and moon gravity assists[J]. Science China-Physics Mechanics & Astronomy, 2015, 58(11): 114501.

Ma PB, Jiang Fanghua, Baoyin HX. Autonomous navigation of Mars probes by combining optical data of viewing Martian moons and SST data[J]. Journal of Navigation, 2015, 68(6): 1019-1040.

Li JY, Gong SP, Baoyin HX, Jiang Fanghua. Lunar orbit insertion targeting from the two-segment lunar free-return trajectories[J]. Advances in Space Research, 2015, 55(4): 1051-1060.

Gong SP, Li JF, Jiang Fanghua. Interplanetary trajectory design for a hybrid propulsion system[J]. Aerospace Science and Technology, 2015, 45: 104-113.

李俊峰, 宝音贺西, 蒋方华. 深空探测动力学与控制[M]. 北京: 清华大学出版社, 2014.

Wu ZG, Jiang Fanghua, Li JF. Artificial Martian frozen orbits and Sun-Synchronous orbits using continuous low-thrust control[J]. Astrophysics and Space Science, 2014, 352(2): 503-514.

He J, Gong SP, Jiang Fanghua, Li JF. Time-optimal rendezvous transfer trajectory for restricted cone-angle range solar sails[J]. Acta Mechanica Sinica, 2014, 30(5): 628-635.

Guo TD, Li JF, Baoyin HX, Jiang Fanghua. Pseudospectral methods for trajectory optimization with interior point constraints: verification and applications[J]. IEEE Transactions on Aerospace and Electronic Systems, 2013, 49(3): 2005-2017.

Jiang Fanghua, Baoyin HX, Li JF. Practical techniques for low-thrust trajectory optimization with homotopic approach[J]. Journal of Guidance Control and Dynamics, 2012, 35(1): 245-258.

Guo TD, Jiang Fanghua, Li JF. Homotopic approach and pseudospectral method applied jointly to low thrust trajectory optimization[J]. Acta Astronautica, 2012, 71: 38-50.

李俊峰, 蒋方华. 连续小推力航天器的深空探测轨道优化方法综述[J]. 力学与实践, 2011, 33(3): 1-6.

蒋方华, 陈杨, 刘跃聪, 宝音贺西, 李俊峰. 2010年国际深空探测轨道优化竞赛的清华大学解法[J]. 力学与实践, 2011, 33(3): 103-105.

Guo TD, Jiang Fanghua, Baoyin HX, Li JF. Fuel optimal low thrust rendezvous with outer planets via gravity assist[J]. Science China-Physics Mechanics & Astronomy, 2011, 54(4): 756-769.

雪丹, 李俊峰, 蒋方华. 卫星在轨道平面内的可达范围研究[J]. 力学学报, 2010, 42(2): 337-342.

Xue D, Li JF, Baoyin HX, Jiang Fanghua. Reachable domain for spacecraft with a single impulse[J]. Journal of Guidance Control and Dynamics, 2010, 33(3): 934-942.

蒋方华, 李俊峰, 宝音贺西. 基于不同天文标准计算地球引力对卫星轨道的影响[J]. 空间控制技术与应用, 2009(2): 38-41.

Zhu KJ, Jiang Fanghua, Li JF, Baoyin HX. Trajectory optimization of multi-asteroids exploration with low thrust[J]. Transactions of the Japan Society for Aeronautical and Space Sciences, 2009, 52(175): 47-54.

Jiang Fanghua, Li JF, Baoyin HX, Gao YF. Two-point boundary value problem solutions to spacecraft formation flying[J]. Journal of Guidance Control and Dynamics, 2009, 32(6): 1827-1837.

Jiang Fanghua, Li JF, Baoyin HX, Gao YF. Study on relative orbit geometry of spacecraft formations in elliptical reference orbits[J]. Journal of Guidance Control and Dynamics, 2008, 31(1): 123-134.

Jiang Fanghua, Li JF, Baoyin HX. Approximate analysis for relative motion of satellite formation flying in elliptical orbits[J]. Celestial Mechanics & Dynamical Astronomy, 2007, 98(1): 31-66.