Multi-rate cubature Kalman filter based data fusion method with residual compensation to adapt to sampling rate discrepancy in attitude measurement system

被引:15
作者
Guo, Xiaoting [1 ]
Sun, Changku [1 ,2 ]
Wang, Peng [1 ,2 ]
机构
[1] Tianjin Univ, State Key Lab Precis Measuring Technol & Instrume, Weijin Rd, Tianjin 300072, Peoples R China
[2] Luoyang Inst Electroopt Equipment, Sci & Technol Electroopt Control Lab, Luoyang 471009, Peoples R China
基金
中国国家自然科学基金;
关键词
MULTISENSOR DYNAMIC-SYSTEMS; MISSING MEASUREMENTS; VISION; MOTION; NAVIGATION;
D O I
10.1063/1.4997072
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
This paper investigates the multi-rate inertial and vision data fusion problem in nonlinear attitude measurement systems, where the sampling rate of the inertial sensor is much faster than that of the vision sensor. To fully exploit the high frequency inertial data and obtain favorable fusion results, a multi-rate CKF (Cubature Kalman Filter) algorithm with estimated residual compensation is proposed in order to adapt to the problem of sampling rate discrepancy. During inter-sampling of slow observation data, observation noise can be regarded as infinite. The Kalman gain is unknown and approaches zero. The residual is also unknown. Therefore, the filter estimated state cannot be compensated. To obtain compensation at these moments, state error and residual formulas are modified when compared with the observation data available moments. Self-propagation equation of the state error is established to propagate the quantity from the moments with observation to the moments without observation. Besides, a multiplicative adjustment factor is introduced as Kalman gain, which acts on the residual. Then the filter estimated state can be compensated even when there are no visual observation data. The proposed method is tested and verified in a practical setup. Compared with multi-rate CKF without residual compensation and single-rate CKF, a significant improvement is obtained on attitude measurement by using the proposed multi-rate CKF with inter-sampling residual compensation. The experiment results with superior precision and reliability show the effectiveness of the proposed method. Published by AIP Publishing.
引用
收藏
页数:11
相关论文
共 32 条
[1]  
[Anonymous], AEU INT J ELECT COMM
[2]   Cubature Kalman Filters [J].
Arasaratnam, Ienkaran ;
Haykin, Simon .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2009, 54 (06) :1254-1269
[3]   Fast ego-motion estimation with multi-rate fusion of inertial and vision [J].
Armesto, Leopoldo ;
Tornero, Josep ;
Vincze, Markus .
INTERNATIONAL JOURNAL OF ROBOTICS RESEARCH, 2007, 26 (06) :577-589
[4]   Combining Stereo Vision and Inertial Navigation System for a Quad-Rotor UAV [J].
Carrillo, Luis Rodolfo Garcia ;
Dzul Lopez, Alejandro Enrique ;
Lozano, Rogelio ;
Pegard, Claude .
JOURNAL OF INTELLIGENT & ROBOTIC SYSTEMS, 2012, 65 (1-4) :373-387
[5]   Three-dimensional motion and structure estimation using inertial sensors and computer vision for augmented reality [J].
Chai, L ;
Hoff, WA ;
Vincent, T .
PRESENCE-TELEOPERATORS AND VIRTUAL ENVIRONMENTS, 2002, 11 (05) :474-492
[6]  
Efe M., 1999, AM CONTR C JUN, P63913
[7]   A Quaternion-Based Unscented Kalman Filter for Robust Optical/Inertial Motion Tracking in Computer-Assisted Surgery [J].
Enayati, Nima ;
De Momi, Elena ;
Ferrigno, Giancarlo .
IEEE TRANSACTIONS ON INSTRUMENTATION AND MEASUREMENT, 2015, 64 (08) :2291-2301
[8]   FlightTracker: A novel optical/inertial tracker for cockpit enhanced vision [J].
Foxlin, E ;
Altshuler, Y ;
Naimark, L ;
Harrington, M .
ISMAR 2004: THIRD IEEE AND ACM INTERNATIONAL SYMPOSIUM ON MIXED AND AUGMENTED REALITY, 2004, :212-221
[9]   Design of multi-sensor attitude determination systems [J].
Gebre-Egziabher, D .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2004, 40 (02) :627-649
[10]   Model-reduced fault detection for multi-rate sensor fusion with unknown inputs [J].
Geng, Hang ;
Liang, Yan ;
Yang, Feng ;
Xu, Linfeng ;
Pan, Quan .
INFORMATION FUSION, 2017, 33 :1-14