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