Universitat Politècnica de Catalunya. Doctorat en Teoria del Senyal i Comunicacions
Universitat Politècnica de Catalunya. Departament de Teoria del Senyal i Comunicacions
Universitat Politècnica de Catalunya. RSLAB - Grup de Recerca en Teledetecció
2021
The advent of geosynchronous remote sensing missions requires the development of precise orbit determination techniques at high orbits. Geosynchronous satellites require station-keeping manoeuvres to be performed periodically. Dynamical models do not consider artificial forces. Therefore, the tracking system must be able to detect them in order to keep track of the spacecraft autonomously. A compact baseline interferometer is deployed in order to track the signals of opportunity from the ASTRA 19.2?E geostationary constellation. The system is capable of autonomously estimate the trajectory of the satellite for a period of 22 days. Even after artificial orbital manoeuvres are performed. These results show that interferometry is a valid alternative for future geosynchronous remote sensing missions which require precise orbit determination. © 2021 IEEE
This work has been supported by the Spanish Science, Research and Innovation Plan (MINECO) with Project Codes TIN2014-55413-C2-1-P and TEC2017-85244-C2-2-P and by Unidad de Excelencia Maria de Maeztu MDM-2016-0600 financed by the Agencia Estatal de Investigacion, Spain.
Peer Reviewed
Postprint (published version)
Conference lecture
English
Àrees temàtiques de la UPC::Enginyeria de la telecomunicació; Remote sensing; Artificial satellites; Artificial satellites in remote sensing; Space vehicles; Tracking; Snow; Low earth orbit satellites; Orbits; Trajectory; Remote sensing; Teledetecció; Satèl·lits artificials; Satèl·lits artificials en teledetecció
Institute of Electrical and Electronics Engineers (IEEE)
https://ieeexplore.ieee.org/document/9553709
Restricted access - publisher's policy
E-prints [72987]