Title :
Research of multi-satellite synchronous orbit determination based on serial integration
Author :
Zhang, Ke ; Zhou, Feng-qi ; Xiong, Jing
Author_Institution :
Inst. of Astronaut., Northwestern Polytech. Univ., Xi´´an, China
Abstract :
Great resources of monitoring and control have been saved in orbit determination for satellite constellation based on satellite-to-satellite and earth-to-satellite tracking, the tracking would have broad application prospects in future constellation and rendezvous and docking of manned space vehicle. The key technologies in multi-satellite precision orbit determination with inter-satellite-link (ISL) are described in the paper. Inter-satellite-link measuring model is established, and precise orbit determination method for multi-satellites and its corresponding formula partial derivative are proposed in the article. The orbit determination software programming is simplified, and clears the multi-satellite and multi-arc orbit determination process, then applies to satellite constellation YaoGan-9. Through the actual task tracking, results show that the method can completely meet the multi-satellite orbit determination application requirement based on earth-to-satellite and satellite-to-satellite tracking.
Keywords :
satellite links; satellite tracking; earth-to-satellite tracking; intersatellite-link; multisatellite orbit determination application requirement; multisatellite synchronous orbit determination; satellite constellation; satellite-to-satellite tracking; serial integration; Atmospheric modeling; Extraterrestrial measurements; Mathematical model; Orbits; Satellite constellations; Satellites; Software; earth-to-satellite tracking; inter-satellite-link; multi-satellite orbit determination; precision analysis; satellite-to-satellite tracking; serial integration;
Conference_Titel :
Multimedia Technology (ICMT), 2011 International Conference on
Conference_Location :
Hangzhou
Print_ISBN :
978-1-61284-771-9
DOI :
10.1109/ICMT.2011.6002407