Citation: | Guochao Fan, Dan Song, Chengdong Xu. Modified Observation Model in Tightly-Coupled INS/GPS Integration[J].JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2017, 26(1): 16-28.doi:10.15918/j.jbit1004-0579.201726.0104 |
[1] |
Luo Jianjun, Ma Weihua, Yuan Jianping, et al. Principles and applications of integrated navigation[M].Xi'an:Northwestern Polytechnical University Press, 2012. (in Chinese)
|
[2] |
Zhou Junchuan, Knedlik Stefan, Loffeld Otmar. INS/GPS tightly-coupled integration using adaptive unscented particle filter[J]. Journal of Navigation, 2010, 63:491-511.
|
[3] |
Geng Yanrui, Wang Jinling. Adaptive estimation of multiple fading factorsin Kalman filter for navigation applications[J]. GPS Solutions, 2008, 12:273-279.
|
[4] |
Mohamed H, Schwarz K P. Adaptive Kalman filtering for INS/GPS[J].Journal of Geodesy,1999, 73:193-203.
|
[5] |
Liang Yueqian, Jia Yingmin. A nonlinear quaternion-based fault-tolerant SINS/GNSS integrated navigation method for autonomous UAVs[J]. Aerospace Science and Technology, 2015, 40:191-199.
|
[6] |
Chang Guobin. Loosely coupled INS/GPS integration with constant lever arm using marginal unscented Kalman filter[J]. Journal of Navigation, 2014, 67:419-436.
|
[7] |
Zhou Junchuan, Knedlik Stefan, Loffeld Otmar. INS/GPS tightly-coupled integration using adaptive unscented particle filter[J]. Journal of Navigation,2010, 63:491-511.
|
[8] |
Meng Yang, Gao Shensheng, Zhong Yongmin, et al. Covariance matching based adaptive unscented Kalman filter for direct filtering in INS/GNSS integration[J]. Acta Astronautica, 2016, 120:171-181.
|
[9] |
Gong Xiaolin, Zhang Jianxu, Fang Jiancheng. A modified nonlinear two-filter smoothing for high-precision airborne integrated GPS and inertial navigation[J]. IEEE Transactions on Instrumentation & Measurement, 2015, 64(12):1-1.
|
[10] |
Tseng Chien-Hao,Lin Sheng-Fuu, Jwo Dah-Jing. Fuzzy adaptive cubature Kalman filter for integrated navigation systems[J]. Sensors, 2016, 16(8):1167.
|
[11] |
Ding Weidong, Wang Jinling, Rizos Chris, et al. Improving adaptive Kalman estimation in GPS/INS integration[J]. Journal of Navigation, 2007, 60(3):517-529.
|
[12] |
Jwo Dah-Jing, Yang Chi-Fan, Chuang Chih-Hsun, et al. A novel design for the ultra-tightly coupled GPS/INS navigation system[J]. Journal of Navigation, 2012, 65:717-747.
|
[13] |
Yu Myeong-Jong. INS/GPS integration system using adaptive filterfor estimating measurement noise variance[J].IEEE Transactions on Aerospace and Electronic Systems, 2012, 48(2):1786-1792.
|
[14] |
Gao Zhouzheng, Shen Wenbin, Zhang Hongping, et al. Application of Helmert variance component based adaptive Kalman filter in multi-GNSS PPP/INS tightly coupled integration[J]. Remote Sensing, 2016, 8(7):553.
|
[15] |
Jwo Dah-Jing, Yang Chi-Fan, Chuang Chih-Hsun, et al. Performance enhancement for ultra-tight GPS/INS integration using a fuzzy adaptive strong tracking unscented Kalman filter[J]. Nonlinear Dynamics, 2013, 73(1-2):377-395.
|
[16] |
Hofmann Wellenhof, Lichtenegger Wasle. GNSS-global navigation satellite systems GPS, GLONASS, Galileo & more[M]. Berlin:Springer-Verlag, 2008.
|
[17] |
Liu Rui. Study on INS/GNS/CNS integrated navigation system of aerocraft[D]. Harbin:Harbin Institute of Technology,2011. (in Chinese)
|