Low-thrust de-orbiting from Low Earth Orbit through natural perturbations

How to enhance end-of-life deorbiting by using orbit perturbations? Check this out in the Open Access paper by Simeng Huang, Camilla Colombo, Elisa Maria Alessi, Yang Wang and Zhili Hou

Quasi optimal semi-analytical law coupled with the leveraging of the resonances between solar radiation pressure and the Earth’s oblateness to produce maps that defines the best condition for de-orbit corridors with low-thrust propulsion. A solution for the end-of-life of large constellations.