Year: 2024
Type: article
Abstract: The circular restricted three-body problem (CR3BP) is analyzed to introduce additional factors into the dynamic model, such as radiation forces, flattening of the primary bodies, relativity effects, and the presence of natural satellites. The introduction of these factors increases the accuracy when obtaining the position of the Lagrange points and the basins of convergence of the system. The Newton–Raphson methodis used to implement a searching algorithm. Finally, an application to the Sun–Mars system including the presence of Phobos and Deimos is developed.
Source: Applied Sciences
DOI: 10.3390/app15010106
Authors: Alicia Herrero, Santiago Moll-Lopez, José-A. Moraño, Erika Vega-Fleitas, Daniel Villalibre
Institution: Universitat Politècnica de València
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: gold
Estimated APC paid: $2,728
Awards: G7499741631, G8219391473
OpenAlex ID: W4405808750