Specificity of simulation and procedure of optimization of SC flight trajectories with a rotor solar sail, including multiple gravity-assist maneuvers

Space technics and technology


Аuthors

Kasmerchuk P. V.

Lavochkin Research and Production Association, NPO Lavochkin, 24, Leningradskay str., Khimki, Moscow region, 141400, Russia

e-mail: pavel.kazmerchuk@gmail.com

Abstract

Specificity of simulation and procedure of optimization of SC flight trajectories with a rotor solar sail, including multiple gravity-assist maneuvers is considered. The problem of optimization of SC flight trajectories with a rotor solar sail is defined as a problem of optimization of compound dynamic system, which is decided by the method of sequential linearization, is proposed.


Download

mai.ru — informational site MAI

Copyright © 2000-2021 by MAI

Вход