Simulation of Earth's Protection by Solar Sail from Asteroid Hazard

被引：0

作者：

Nikolaeva, Elizaveta ^{[1
]}

Starinova, Olga ^{[1
]}

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

Alipova, B. ^{[2
]}

机构：

[1] Samara Natl Res Univ, Dept Space Engn, Samara, Russia

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

来源：

2018 IEEE 12TH INTERNATIONAL CONFERENCE ON APPLICATION OF INFORMATION AND COMMUNICATION TECHNOLOGIES (AICT) | 2018年

关键词：

asteroid; solar sail; mathematical model; dangerous orbit; software package;

D O I：

暂无

中图分类号：

TP301 [理论、方法];

学科分类号：

081202 ;

摘要：

The present work is devoted to one of the methods of the Earth's protection from asteroid danger, namely, the use of the solar sail - a spacecraft, with the additional lighting the repels an asteroid from a dangerous orbit. The parameters of the near-Earth asteroids are revealed. Mathematical model of the control movement of all bodies (the Earth, the Sun, the asteroid, the solar sail), the control program and the software package (Delphi 7) for the simulation and visualization of the trajectories are designed.

引用

页码：340 / 343

页数：4

共 8 条

[1]

[Anonymous], 2009, P INT S NEAR EARTH H, V48, p[387, 377]

[2]

Boyarchuk A. A., 1999, COMINFORM

[3]

Eneev T. M., 2011, 35 IPM MV KELD, P40

[4]

Finkelstein A., 2010, P INT C ASTEROIDCOME

[5]

Gorbunova I. V., 2017, Computer program, Russia, the patent, Patent No. 2017662592

[6] An approach for the control method's determination for an interplanetary mission with solor sail [J].

Gorbunova, Irina ;

Starinova, Olga .

ICNPAA 2016 WORLD CONGRESS: 11TH INTERNATIONAL CONFERENCE ON MATHEMATICAL PROBLEMS IN ENGINEERING, AEROSPACE AND SCIENCES, 2017, 1798

[7]

Sokolsky A. G., 1996, ASTEROID COMET HAZAR, P244

[8]

Zubrin D. S., 1999, HORIZON POSSIBLE J

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