System of artificial intellect support of low-thrust spacecraft interplanetary mission optimization

Abstract


The paper deals with an information computational system of artificial intellect support of low-thrust interplanetary ion optimization. By mission optimization is meant joint optimization of lows of control as well as spacecraft motion trajectories and design parameters which correspond to them. The system is based on the use of up-to-date dynamic data processing methods obtained on the sequence of refined mission models.


About the authors

O. L. Starinova

Samara State Aerospace University

Author for correspondence.
Email: starinova@ssau.ru

Russian Federation

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