State Vector Determination By A Single Tracking Satellite
Astrophysics
2022-08-29 v2
Abstract
Using only a single tracking satellite capable of only range measurements to an orbiting object in an unknown Keplerian orbit, it is theoretically possible to calculate the orbit and a current state vector. In this paper we derive an algorithm that can perform this calculation.
Cite
@article{arxiv.0705.1155,
title = {State Vector Determination By A Single Tracking Satellite},
author = {Kerry M. Soileau},
journal= {arXiv preprint arXiv:0705.1155},
year = {2022}
}