Fanghua Jiang
Tsinghua University
My Publications
Optimization of Variable-Specific-Impulse Gravity-Assist Trajectories
Journal of Spacecraft and Rockets
March 2020
Real-time control for fuel-optimal Moon landing based on an interactive deep reinforcem...
Astrodynamics
July 2019
A simple method to design non-collision relative orbits for close spacecraft formation ...
Science China Physics Mechanics and Astronomy
March 2018
Fuel-Optimal Low-Thrust Trajectory Optimization Using Indirect Method and Successive Co...
IEEE Transactions on Aerospace and Electronic Systems
January 2018
Dynamics and control for contactless interaction between spacecraft and tumbling debris
Advances in Space Research
January 2018
悬挂点匀速转动时摆锤圆周运动的存在性与稳定性分析
应用数学和力学
January 2018
Improving Low-Thrust Trajectory Optimization by Adjoint Estimation with Shape-Based Path
Journal of Guidance Control and Dynamics
December 2017
Optimization of observing sequence based on nominal trajectories of symmetric observing...
Astrodynamics
September 2017
Autonomous Navigation of Mars Probes by Single X-ray Pulsar Measurement and Optical Dat...
Journal of Navigation
July 2016
Systematic low-thrust trajectory optimization for a multi-rendezvous mission using adjo...
Astrophysics and Space Science
March 2016
Capture of near-Earth objects with low-thrust propulsion and invariant manifolds
Astrophysics and Space Science
December 2015
Extension of frozen orbits and Sun-synchronous orbits around terrestrial planets using ...
Astrophysics and Space Science
October 2015
Low-thrust trajectory optimization of asteroid sample return mission with multiple revo...
Science China Physics Mechanics and Astronomy
October 2015
Interplanetary trajectory design for a hybrid propulsion system
Aerospace Science and Technology
September 2015
Autonomous Navigation of Mars Probes by Combining Optical Data of Viewing Martian Moons...
Journal of Navigation
April 2015
Asteroid body-fixed hovering using nonideal solar sails
Research in Astronomy and Astrophysics
March 2015
Lunar orbit insertion targeting from the two-segment lunar free-return trajectories
Advances in Space Research
February 2015
Study on the connection between the rotating mass dipole and natural elongated bodies
Astrophysics and Space Science
December 2014
Time-optimal rendezvous transfer trajectory for restricted cone-angle range solar sails
Acta Mechanica Sinica
October 2014
Artificial Martian frozen orbits and Sun-Synchronous orbits using continuous low-thrust...
Astrophysics and Space Science
May 2014
Pseudospectral Methods for Trajectory Optimization with Interior Point Constraints: Ver...
IEEE Transactions on Aerospace and Electronic Systems
July 2013
Homotopic approach and pseudospectral method applied jointly to low thrust trajectory o...
Acta Astronautica
February 2012
Practical Techniques for Low-Thrust Trajectory Optimization with Homotopic Approach
Journal of Guidance Control and Dynamics
January 2012
Fuel optimal low thrust rendezvous with outer planets via gravity assist
Science China Physics Mechanics and Astronomy
March 2011
Reachable Domain for Spacecraft with a Single Impulse
Journal of Guidance Control and Dynamics
May 2010
Two-Point Boundary Value Problem Solutions to Spacecraft Formation Flying
Journal of Guidance Control and Dynamics
November 2009
Trajectory Optimization of Multi-Asteroids Exploration with Low Thrust
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
January 2009
Study on Relative Orbit Geometry of Spacecraft Formations in Elliptical Reference Orbits
Journal of Guidance Control and Dynamics
January 2008
Approximate analysis for relative motion of satellite formation flying in elliptical or...
Celestial Mechanics and Dynamical Astronomy
April 2007
