Iterative Methods of Ballistic Schemes Optimization
of Interplanetary Mission with Low Thrust
Researches of planets, interplanetary and circumsolar space give the chance to receive answers to many fundamental questions and to use astronautics achievements by working out of practically unlimited resources of Solar system. Programs of studying of space demand the big material inputs and do not give fast return. Use of perspective electro propulsion systems allows to raise efficiency of the created and developed space technology. In the decision of a problem of increase scientific and economic efficiency of space researches the important role is played by the complex optimization of mission including definition of optimum structure and parameters of space vehicles systems, control optimum programs and movement trajectories corresponding to them. Given article is devoted this problem.