Fanghua Jiang

  • Tsinghua University

My Publications

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