A Civil Aviation Oriented SINS/DGPS Fusion Method for Integrated Navigation

HU Jie; YAN Yongjie; SHI Xiaozhu

doi:10.3969/j.issn.1671-637x.2020.04.008

[2] LEE J, PULLEN S, DATTA-BARUA S, et al.Real-time ionospheric threat adaptation using a space weather prediction for GNSS-based aircraft landing systems［J］.IEEE Transactions on Intelligent Transportation Systems, 2017, 18(7): 1752-1761.

LEE J, PULLEN S, DATTA-BARUA S, et al.Real-time ionospheric threat adaptation using a space weather prediction for GNSS-based aircraft landing systems［J］.IEEE Transactions on Intelligent Transportation Systems, 2017, 18(7): 1752-1761.

[3] FELUX M, DAUTERMANN T, BECKER H.GBAS approach guidance performance-a comparison to ILS［C］// Proceedings of the International Technical Meeting of the Institute of Navigation, 2013: 4-9.

FELUX M, DAUTERMANN T, BECKER H.GBAS approach guidance performance-a comparison to ILS［C］// Proceedings of the International Technical Meeting of the Institute of Navigation, 2013: 4-9.

[4] ENGE P.Local area augmentation of GPS for the precision approach of aircraft［J］.Proceedings of the IEEE, 1999, 87(1): 111-132.

ENGE P.Local area augmentation of GPS for the precision approach of aircraft［J］.Proceedings of the IEEE, 1999, 87(1): 111-132.

[5] DAUTERMANN T, FELUX M, GROSCH A.Approach service type D evaluation of the DLR GBAS testbed［J］.GPS Solutions, 2012, 16(3): 375-387.

DAUTERMANN T, FELUX M, GROSCH A.Approach service type D evaluation of the DLR GBAS testbed［J］.GPS Solutions, 2012, 16(3): 375-387.

[6] DAUTERMANN T, MAYER C, ANTREICH F, et al.Non-Gaussian error modeling for GBAS integrity assessment［J］.IEEE Transactions on Aerospace and Electronic Systems, 2012, 48(1): 693-706.

DAUTERMANN T, MAYER C, ANTREICH F, et al.Non-Gaussian error modeling for GBAS integrity assessment［J］.IEEE Transactions on Aerospace and Electronic Systems, 2012, 48(1): 693-706.

[7] CIRCIU M S, MEURER M, FELUX M, et al.Evaluation of GPS L5 and Galileo E1 and E5a performance for future multi-frequency and multi-constellation GBAS［J］.Journal of the Institute of Navigation, 2017, 64(1): 149-163.

CIRCIU M S, MEURER M, FELUX M, et al.Evaluation of GPS L5 and Galileo E1 and E5a performance for future multi-frequency and multi-constellation GBAS［J］.Journal of the Institute of Navigation, 2017, 64(1): 149-163.

[9] XING Z D, ZHAO J B, WANG Z H, et al.Analysis and improvement to ionosphere grads integrity monitoring algorithm in ground based augmentation system［C］//Proceedings of Chinese Satellite Navigation Conference(CSNC), 2015: 237-247.

XING Z D, ZHAO J B, WANG Z H, et al.Analysis and improvement to ionosphere grads integrity monitoring algorithm in ground based augmentation system［C］//Proceedings of Chinese Satellite Navigation Conference(CSNC), 2015: 237-247.

[10] HU J, SUN Q W, SHI X Z.Differential positioning algorithm for GBAS based on extended Kalman filtering［C］//Proceedings of the 13th World Congress on Inte-lligent Control and Automation(WCICA), 2018: 296-303.

HU J, SUN Q W, SHI X Z.Differential positioning algorithm for GBAS based on extended Kalman filtering［C］//Proceedings of the 13th World Congress on Inte-lligent Control and Automation(WCICA), 2018: 296-303.

[11] WANG Z P, MACABIAU C, ZHANG J, et al.Prediction and analysis of GBAS integrity monitoring availability at LinZhi airport［J］.GPS Solutions, 2014, 18(1): 27-40.

WANG Z P, MACABIAU C, ZHANG J, et al.Prediction and analysis of GBAS integrity monitoring availability at LinZhi airport［J］.GPS Solutions, 2014, 18(1): 27-40.

[12] HUANG Z G, HUANG Z G, ZHU Y B.A new optimal Hatch filter to minimize the effects of ionosphere gradients for GBAS［J］.Chinese Journal of Aeronautics, 2008, 21(6): 526-532.

HUANG Z G, HUANG Z G, ZHU Y B.A new optimal Hatch filter to minimize the effects of ionosphere gradients for GBAS［J］.Chinese Journal of Aeronautics, 2008, 21(6): 526-532.

[13] Federal Aviation Administration.Roadmap for perfor-mance-based navigation［Z］.Washington, DC.: Federal Aviation Administration, 2006.

［14］CHAN F C.A state dynamics method for integrated GPS/INS navigation and its application to aircraft precision approach［D］.Chicago: Illinois Institute of Techno-logy, 2008.

Federal Aviation Administration.Roadmap for perfor-mance-based navigation［Z］.Washington, DC.: Federal Aviation Administration, 2006.

［14］CHAN F C.A state dynamics method for integrated GPS/INS navigation and its application to aircraft precision approach［D］.Chicago: Illinois Institute of Techno-logy, 2008.

[16] GROSCH A, BELABBAS B, MEURER M.Redundant inertial-aided GBAS for civil aviation［C］//Proceedings of the 5th ESA Workshop on Satellite Navigation Technologies and European Workshop on GNSS Signals and Signal Processing (NAVITEC), 2010: 1-6.]

GROSCH A, BELABBAS B, MEURER M.Redundant inertial-aided GBAS for civil aviation［C］//Proceedings of the 5th ESA Workshop on Satellite Navigation Technologies and European Workshop on GNSS Signals and Signal Processing (NAVITEC), 2010: 1-6.]