The Simulation of the Interplanetary Travel of the Solar Sail Spacecraft to the Potentially Hazardous Asteroid
- https://doi.org/10.2991/eers-15.2015.30How to use a DOI?
- spacecraft; solar sail; potentially hazardous asteroid; mathematical motion model; heliocentric coordinate system; motion simulation
This paper discusses interplanetary travel, especially flight to the asteroids, by means of spacecraft which use solar sail instead of an engine and a propellant. The design model of the solar sail spacecraft “Helios” which created in computer-aided design system is described. The mathematical motion model for such type of spacecraft is considered and used for motion simulation session. The simulation of flight to the potentially hazardous asteroid is performed with the aid of special software complex which is developed for the purpose of this work
- © 2015, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Roman M. Khabibullin AU - Olga L. Starinova PY - 2015/09 DA - 2015/09 TI - The Simulation of the Interplanetary Travel of the Solar Sail Spacecraft to the Potentially Hazardous Asteroid BT - Proceedings of the 2015 International Conference on Environmental Engineering and Remote Sensing PB - Atlantis Press SP - 122 EP - 125 SN - 2352-538X UR - https://doi.org/10.2991/eers-15.2015.30 DO - https://doi.org/10.2991/eers-15.2015.30 ID - Khabibullin2015/09 ER -