System synthesis of optimum interplanetary trajectories on the basis of modern space technologies.

Аuthors

Usachov V. E.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

e-mail: usachov@inbox.ru

Abstract

The system approach of synthesis of optimum interplanetary trajectories on the basis of modern space technologies for a wide range of the distant space missions planned for immediate prospects is offered. High power possibilities of received interplanetary trajectories and rather low cost of space missions are reached at the expense of use of repeated gravitational maneuvers at planets and application of electrojet engines. For the decision of a challenge of optimum control of compound dynamic system with functional restrictions the original technique is offered.

Keywords:

an interplanetary trajectory, distant space mission, gravitational maneuvers, electrojet engines, optimization, management, compound dynamic system, functionals, restrictions

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