TY - GEN
T1 - Study on attitude measurement in gyro-free inertial navigation system
AU - Wang, Xiaoli
AU - Zhou, Xun
PY - 2011
Y1 - 2011
N2 - Through analysing the measurement priniple 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.
AB - Through analysing the measurement priniple 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.
KW - Acceleromete
KW - Attitude measurement
KW - GFSINS
UR - https://www.scopus.com/pages/publications/80054812889
U2 - 10.1109/MACE.2011.5987989
DO - 10.1109/MACE.2011.5987989
M3 - Conference contribution
AN - SCOPUS:80054812889
SN - 9781424494392
T3 - 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011 - Proceedings
SP - 4432
EP - 4434
BT - 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011 - Proceedings
T2 - 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011
Y2 - 15 July 2011 through 17 July 2011
ER -