@inproceedings{50df28d64d0f442db2b1a495054e5bcc,
title = "Spacecraft inertial navigation errors nearby perigee and its elimination",
abstract = "A practical problem on spacecraft inertial navigation system (INS) is described in the paper. Inertial Navigation System using in an elliptical orbit spacecraft causes a huge error when the spacecraft close to the perigee, The Causes for this error are discussed and the scale of it is estimated by simulation. Methods of eliminating the error are studied: the integrated navigation method and the compensation of initial orbit calculation method. Simulation results verify the validity of the proposed methods.",
keywords = "INS error at perigee, Initial orbit calculation, Integrated navigation, Spacecraft navigation",
author = "Pu, \{Jia Iun\} and Cui, \{Nai Gang\} and Zhang, \{Li Bin\}",
year = "2009",
doi = "10.1109/ICMA.2009.5244823",
language = "英语",
isbn = "9781424426935",
series = "2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009",
pages = "4539--4543",
booktitle = "2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009",
note = "2009 IEEE International Conference on Mechatronics and Automation, ICMA 2009 ; Conference date: 09-08-2009 Through 12-08-2009",
}