2009, Ph.D. Mechanics, Tsinghua University;

2004, BE Engineering Mechanics, Tsinghua University

12/2014—present, Associate Professor, School of Aerospace Engineering, Tsinghua University

6/2011—11/2014, Assistant Researcher, School of Aerospace Engineering, Tsinghua University

7/2009—5/2011, Postdoctor, School of Aerospace Engineering, Tsinghua University

AIAA Senior Member

Associate Editor of Astrodynamics

Astrodynamics and control

Low-thrust interplanetary trajectory optimization

2009—Excellent Ph.D. graduate (4%) and PhD dissertation of Tsinghua University

2010—Champion of the 2nd Chinese Space Orbit Design Competition (the key member of Tsinghua University team)

2010—Second runner-up of the 5th Global Trajectory Optimization Competition (the key member of Tsinghua University team)

2015—Runner-up of the 8th Global Trajectory Optimization Competition (the only coach of Tsinghua University team)

[1] Jiang Fanghua; Tang Gao. Systematic low-thrust trajectory optimization for a multi-rendezvous mission using adjoint scaling. Astrophysics and Space Science, 2016, 361(4): No. 117.

[2] Tang, Gao; Jiang, Fanghua. Capture of near-Earth objects with low-thrust propulsion and invariant manifolds. Astrophysics and Space Science, 2016, 361: 10.

[3] Tang Gao; Yang Hongwei; Jiang Fanghua; Baoyin Hexi; Li Junfeng. GTOC8: Results and methods of team 3 - Tsinghua university，26th AAS/AIAA Space Flight Mechanics Meeting, Napa, CA, United States, 2016.

[4] 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): No. 114501.

[5] Zeng Xiangyuan; Jiang Fanghua; Li Junfeng. Asteroid body-fixed hovering using nonideal solar sails. Research in Astronomy and Astrophysics, 2015, 15(4): 597~607.

[6] Zeng, Xiangyuan; Jiang, Fanghua; Li, Junfeng; Baoyin, Hexi. Study on the connection between the rotating mass dipole and natural elongated bodies. Astrophysics and Space Science, 2015, 356(1): 29-42.

[7] Ma, Pengbin; Jiang, Fanghua; Baoyin, Hexi. Autonomous Navigation of Mars Probes by Combining Optical Data of Viewing Martian Moons and SST Data. Journal of Navigation, 2015, 68(6): 1019-1040.

[8] Tang Gao; Jiang Fanghua. Trajectory Optimization for Low-Thrust Multiple Asteroids Rendezvous Mission. 2015 AAS/AIAA Astrodynamics Specialist Conference, Vail, CO, USA, 2015.

[9] 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).

[10] Jiang Fanghua; Chen Yang; Liu Yuecong; Baoyin Hexi; Li Junfeng. GTOC5: Results from the Tsinghua University. Acta Futura, 2014, 8(2): 37-44.

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

[12] Li Junfeng; Baoyin Hexi; Jiang Fanghua. Dynamics and Control of Interplanetary Flight. Beijing, Tsinghua University Press, 2014.

[13] Jiang, Fanghua; Baoyin, Hexi; Li, Junfeng. Practical techniques for low-thrust trajectory optimization with homotopic approach. Journal of Guidance, Control, and Dynamics, 2012, 35: 245-258.

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

[15] Guo Tieding; Jiang Fanghua; Baoyin Hexi; Li Junfeng. Fuel optimal low thrust rendezvous with outer planets via gravity assist. Science China-Physics Mechanics & Astronomy, 2011, 54: 756-769.

[16] Li Junfeng; Jiang Fanghua. Survey of low-thrust trajectory optimization methods for deep space exploration. Mechanics in Engineering, 2011, 33: 1-6.

[17] Zhu Kaijian; Jiang Fanghua; Li Junfeng; Baoyin Hexi. Trajectory optimization of multi-asteroids exploration with low thrust. Transactions of the Japan Society for Aeronautical and Space Sciences, 2009, 52(175): 47~54.

[18] Jiang, Fanghua; Li, Junfeng; Baoyin, Hexi; Gao, Yunfeng. Two-point boundary value problem solutions to spacecraft formation flying. Journal of Guidance, Control, and Dynamics, 2009, 32(6): 1827-1837.

[19] Jiang, Fanghua; Li, Junfeng; Baoyin, Hexi; Gao, Yunfeng. Study on relative orbit geometry of spacecraft formations in elliptical reference orbits. Journal of Guidance, Control, and Dynamics, 2008, 31(1): 123-134.

[20] Jiang, Fanghua; Li, Junfeng; Baoyin, Hexi. Approximate analysis for relative motion of satellite formation flying in elliptical orbits. Celestial Mechanics and Dynamical Astronomy, 2007, 98(1): 31-66.