Angular Motion Estimation Using Dynamic Models in a Gyro-Free Inertial Measurement Unit

被引:15
作者
Edwan, Ezzaldeen [1 ]
Knedlik, Stefan [2 ]
Loffeld, Otmar [1 ]
机构
[1] Univ Siegen, Ctr Sensor Syst ZESS, D-57068 Siegen, Germany
[2] iMAR GmbH, St Ingbert, Germany
关键词
angular motion estimation; GF-IMU; dynamic models; CALIBRATION; TRACKING; VELOCITY; IMU;
D O I
10.3390/s120505310
中图分类号
O65 [分析化学];
学科分类号
070302 ; 081704 ;
摘要
In this paper, we summarize the results of using dynamic models borrowed from tracking theory in describing the time evolution of the state vector to have an estimate of the angular motion in a gyro-free inertial measurement unit (GF-IMU). The GF-IMU is a special type inertial measurement unit (IMU) that uses only a set of accelerometers in inferring the angular motion. Using distributed accelerometers, we get an angular information vector (AIV) composed of angular acceleration and quadratic angular velocity terms. We use a Kalman filter approach to estimate the angular velocity vector since it is not expressed explicitly within the AIV. The bias parameters inherent in the accelerometers measurements' produce a biased AIV and hence the AIV bias parameters are estimated within an augmented state vector. Using dynamic models, the appended bias parameters of the AIV become observable and hence we can have unbiased angular motion estimate. Moreover, a good model is required to extract the maximum amount of information from the observation. Observability analysis is done to determine the conditions for having an observable state space model. For higher grades of accelerometers and under relatively higher sampling frequency, the error of accelerometer measurements is dominated by the noise error. Consequently, simulations are conducted on two models, one has bias parameters appended in the state space model and the other is a reduced model without bias parameters.
引用
收藏
页码:5310 / 5327
页数:18
相关论文
共 16 条
[1]  
Bragge T, 2006, P 1 JOINT ESMAC GCMA
[2]   Estimating the angular velocity of a rigid body moving in the plane from tangential and centripetal acceleration measurements [J].
Cardou, Philippe ;
Angeles, Jorge .
MULTIBODY SYSTEM DYNAMICS, 2008, 19 (04) :383-406
[3]   A Nonlinear Program for Angular-Velocity Estimation From Centripetal-Acceleration Measurements [J].
Cardou, Philippe ;
Fournier, Guillaume ;
Gagnon, Philippe .
IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2011, 16 (05) :932-944
[4]   Constrained Angular Motion Estimation in a Gyro-Free IMU [J].
Edwan, Ezzaldeen ;
Knedlik, Stefan ;
Loffeld, Otmar .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2011, 47 (01) :596-610
[5]  
El-Sheimy N., PROMISE MEMS NAVIGAT
[6]  
Isidori A., 1995, NONLINEAR CONTROL SY, V3rd, DOI 10.1007/978-1-84628-615-5
[7]   Survey of maneuvering target tracking. Part I: Dynamic models [J].
Li, XR ;
Jilkov, VP .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2003, 39 (04) :1333-1364
[8]   Spacecraft attitude/rate estimation using vector-aided GPS observations [J].
Oshman, Y ;
Markley, FL .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1999, 35 (03) :1019-1032
[9]   A scheme for improving the performance of a gyroscope-free inertial measurement unit [J].
Park, S ;
Tan, CW ;
Park, J .
SENSORS AND ACTUATORS A-PHYSICAL, 2005, 121 (02) :410-420
[10]   Design, geometry evaluation, and calibration of a gyroscope-free inertial measurement unit [J].
Schopp, Patrick ;
Klingbeil, Lasse ;
Peters, Christian ;
Manoli, Yiannos .
SENSORS AND ACTUATORS A-PHYSICAL, 2010, 162 (02) :379-387