On fast rendezvous and docking for manned lunar spacecraft

Based on the demand of fast rendezvous and docking of manned lunar mission, it builds the mathematic model and numerical simulation to achieve the fast rendezvous and docking of manned lunar mission. It studies the necessity of spacecraft fast rendezvous and docking, researches on the present status of fast rendezvous and docking of domestic and abroad spacecraft, and obtains the realized conditions. It aims at the earth orbit and lunar orbit fast rendezvous and docking respectively, builds the spacecraft dynamical model, lunar orbit design model and constraint condition, analyzes the launch windows of the fast rendezvous and docking of earth orbit and lunar orbit by means of numerical simulation.