DocumentCode :
2811404
Title :
Study on attitude measurement in gyro-free inertial navigation system
Author :
Wang, Xiaoli ; Zhou, Xun
Author_Institution :
Acad. of Armored Forces Engineerng, Beijing, China
fYear :
2011
fDate :
15-17 July 2011
Firstpage :
4432
Lastpage :
4434
Abstract :
Through analysing the measurement principle of the accelerometer-based gyro-free inertial navigation system, this paper designed a kind of easy to engineering realization of 9 accelerometer configuration scheme, studied attitude measurement principle based on this configuration.Through analysing the acceleration in the carrier movement, obtained angular velocity and linear acceleration.
Keywords :
acceleration measurement; accelerometers; attitude measurement; inertial navigation; accelerometer configuration scheme; accelerometer-based gyrofree inertial navigation system; angular velocity; attitude measurement principle; linear acceleration; Acceleration; Accelerometers; Force measurement; Gyroscopes; Inertial navigation; Instruments; Velocity measurement; Accelerometer; Attitude Measurement; GFSINS;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechanic Automation and Control Engineering (MACE), 2011 Second International Conference on
Conference_Location :
Hohhot
Print_ISBN :
978-1-4244-9436-1
Type :
conf
DOI :
10.1109/MACE.2011.5987989
Filename :
5987989
Link To Document :
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