Study on gyro error correcting for SOTM

Author

Xu, Guimin ; Xu, Huachun ; Chen, Huihua

Author_Institution

Coll. of Marine, Northwestern Polytech. Univ., Xi´´an, China

fYear

2009

Abstract

The factors influence on beam pointing for SOTM were studied. The earth rotation and gyro zero offset were removed based on open loop correcting, three angular rate gyros mounted orthogonally to each other were corrected by four accelerometers, and the scheme applies satellite tracking information to correct gyro error was put forward, the simulation results indicate this method could effectively calibrate error caused by gyro´s long term running.

Keywords

error correction; gyrotrons; mobile satellite communication; satellite antennas; satellite tracking; SOTM; accelerometers; angular rate gyros; earth rotation; gyro error correction; gyro zero offset; gyrotron; mobile satellite technology; open loop correction; satcom on-the-move; satellite antenna; satellite tracking information; Accelerometers; Artificial satellites; Computer errors; Earth; Error correction; Instruments; Military satellites; Satellite antennas; Satellite broadcasting; Tracking loops; AGC; SOTM; accelerometer; earth rotation; error correcting; gyro; null drift; zero offset;

fLanguage

English

Publisher

ieee

Conference_Titel

Electronic Measurement & Instruments, 2009. ICEMI '09. 9th International Conference on

Conference_Location

Beijing

Print_ISBN

978-1-4244-3863-1

Electronic_ISBN

978-1-4244-3864-8

Type

conf

DOI

10.1109/ICEMI.2009.5274882

Filename

5274882