@inproceedings{61ae5567bb3745bea70bfee904fe2854,
title = "Performance discussion on space integrated navigation based three GPS satellites",
abstract = "Facing the probable situation of less four navigation satellites of Global Positioning System (GPS) during the orbit transferring of Space Transfer Vehicle (STV) , the integrated navigation plan from three satellites pesudorange information is supposed and the performance of GPS/Strapdown Inertial Navigation System (SINS) based three GPS satellites is discussed. We construct the SINS space navigation model, derive the navigation errors model of SINS and chose the errors as the states of Kalman Filter. The corresponding Kalman Filter with three pesudorange information is designed. Simulations show that GPS/INS could still supplies better navigation parameters for STV in orbit transferring just with 3 GPS navigation satellites.",
keywords = "GPS/SINS, Global positioning system (GPS), Kalman filter, Space transfer vehicle (STV), Strapdown inertial navigation system (SINS), Three satellites",
author = "Weihua Ma and Jianjun Luo and Mingming Wang and Bo Yang",
year = "2009",
doi = "10.1109/ICEMI.2009.5274315",
language = "英语",
isbn = "9781424438624",
series = "ICEMI 2009 - Proceedings of 9th International Conference on Electronic Measurement and Instruments",
publisher = "IEEE Computer Society",
pages = "326--329",
booktitle = "ICEMI 2009 - Proceedings of 9th International Conference on Electronic Measurement and Instruments",
note = "9th International Conference on Electronic Measurement and Instruments, ICEMI 2009 ; Conference date: 16-08-2009 Through 19-08-2009",
}