Control of the Spacecraft with a Solar Sail, Performing an Interplanetary Flight

被引：0

作者：

Gorbunova, Irina ^{[1
]}

Starinova, Olga ^{[1
]}

机构：

[1] Samara State Aerosp Univ, Space Engn Dept, Samara, Russia

来源：

2015 7TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES (RAST) | 2015年

关键词：

solar sail; controlled movement; center mass; mathematical model; Pontryagin's maximum principle; optimal control; interplanetary flight;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This article is devoted to research of mathematical models and the control of movement of center mass of spacecraft with a solar sail and the movement relative to the center mass of spacecraft. Authors have received the main ballistic parameters and the trajectories of the flights to Venus and Mercury for exact optimal solution and locally-optimal control laws.

引用

页码：111 / 115

页数：5

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