A Low-thrust Spacecraft Propulsion Technology and Its Orbit Transfer Application

For the propulsion technology and orbit transfer control of low-thrust spacecraft, the previous traditional methods and technologies are relatively expensive and cannot guarantee the optimal solution. This paper proposes a new solution method for the low-thrust spacecraft propulsion technology and orbit transfer design, which can optimize the propulsion and orbit transfer flight of low-thrust spacecraft. Theoretical design shows that this method can quickly obtain the optimal analytical solution, and has good optimization effects on the propulsion and orbit transfer of low-thrust spacecraft.