Orbital effects in a cloud of space debris making a close approach with the earth

The present paper has the goal of studying the changes of the orbital parameters of each individual element of a cloud of particles that makes a close approach with the Earth. Clouds of particles are formed when natural or man-made bodies explode for some reason. After an explosion like that, the ce...

Full description

Saved in:
Bibliographic Details
Published in:Computational & applied mathematics 2018-12, Vol.37 (Suppl 1), p.133-143
Main Authors: Formiga, Jorge Kennety S., Gomes, Vivian Martins, de Moraes, Rodolpho Vilhena
Format: Article
Language:English
Subjects:
Applications of Mathematics
Applied physics
Collision dynamics
Computational mathematics
Computational Mathematics and Numerical Analysis
Computer simulation
Conics
Earth
Initial conditions
Maneuvers
Mathematical Applications in Computer Science
Mathematical Applications in the Physical Sciences
Mathematics
Mathematics and Statistics
Missions
Space debris
Trajectories
Citations: Items that this one cites
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Description
Summary:The present paper has the goal of studying the changes of the orbital parameters of each individual element of a cloud of particles that makes a close approach with the Earth. Clouds of particles are formed when natural or man-made bodies explode for some reason. After an explosion like that, the center of mass of the cloud follows the same orbit of the body that generated the explosion, but the individual particles have different trajectories. The cloud is specified by a distribution of semi-major axis and eccentricity of their particles. This cloud is assumed to pass close to the Earth, making a close approach that modifies the trajectory of every particle that belongs to the cloud. The present paper makes simulations based in the “Patched-Conics” model to obtain the new trajectories of each particle. Then, it is possible to map the new distribution of the Keplerian elements of the particles that constituted the cloud, using the previous distribution as initial conditions. These information are important when planning satellite missions having a spacecraft passing close to a cloud of this type, because it is possible to obtain values for the density and amplitude of the cloud, so finding the risks of collision and the possible maneuvers that need to be made in the spacecraft to avoid the collisions.
ISSN:0101-8205
2238-3603
1807-0302
DOI:10.1007/s40314-017-0443-z