Mathematical modeling of solar sail spacecraft guidance by considering the form of surface

被引：0

作者：

Starinova, O. L. ^{[1
]}

Gorbunova, I., V ^{[1
]}

Chekashov, A. S. ^{[1
]}

Bakhyt, Alipova ^{[2
]}

机构：

[1] Samara Univ, Inst Space Rocket Engn, Dept Space Engn, Samara, Russia

[2] Int Informat Technol Univ, Dept Math & Comp Modeling, Alma Ata, Kazakhstan

来源：

PROCEEDINGS OF 8TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES (RAST 2017) | 2017年

关键词：

solar sail; spacecraft; light pressure; osculating elements; heliocentric movement; the trajectory of interplanetary flight; orbit; the ecliptic plane;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The heliocentric motion of the solar sail spacecraft (SSS) is described in classical Keplerian elements. The solar sail with an ideal reflection coefficient is considered. The spacecraft performs a noncoplanar motion with the sun gravity and the light pressure. Disturbances of other celestial bodies gravity are not considered. To confirm the results correctness, we simulated the motion of solar sail spacecraft. The spacecraft's initial orbit coincides with the average Earth orbit relative to the Sun. Authors developed a program complex to simulate the planar heliocentric movement and obtained results for motion simulation of flights to Venus. The results were compared with the simulation results obtained using the Pontryagin maximum principle.

引用

页码：439 / 442

页数：4

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