[1] Jekeli C. Inertial navigation systems with geodetic applications. Inertial Navigation Systems with Geodetic Applications: de Gruyter; 2012.##
[2] Norouz M, Ebrahimi M, Arbabmir M. A Review of Integrated Navigation System GPS/INS Methods and Study of New Approaches in This Field. Journal of Mechanical Engineering. 2018;48(3):365-9..##
[3] M. Norouzi ME, and M. Arbabmir. A review of newly developed algorithms in GPS/INS integration. Int Aerosp Conf iran. 2017.##
[4] Wang M, Wu W, Zhou P, He X. State transformation extended Kalman filter for GPS/SINS tightly coupled integration. Gps Solutions. 2018;22(4):1-12.##
[5] Li T, Zhang H, Gao Z, Chen Q, Niu X. High-accuracy positioning in urban environments using single-frequency multi-GNSS RTK/MEMS-IMU integration. Remote sensing. 2018;10(2):205.##
[6] Li W, Li W, Cui X, Zhao S, Lu M. A Tightly Coupled RTK/INS Algorithmwith Ambiguity Resolution in the Position Domain for Ground Vehicles in Harsh Urban Environments. Sensors (14248220). 2018;18(7).##
[7] Tawk Y, Tomé P, Botteron C, Stebler Y, Farine P-A. Implementation and performance of a GPS/INS tightly coupled assisted PLL architecture using MEMS inertial sensors. Sensors. 2014;14(2):3768-96.##
[8] Wendel J, Trommer GF. Tightly coupled GPS/INS integration for missile applications. Aerospace Science and Technology. 2004;8(7):627-34.##
[9] Falco G, Pini M, Marucco G. Loose and tight GNSS/INS integrations: Comparison of performance assessed in real urban scenarios. Sensors. 2017;17(2):255.##
[10] Houzeng H, Jian W, Mingyi D. GPS/BDS/INS tightly coupled integration accuracy improvement using an improved adaptive interacting multiple model with classified measurement update. Chinese Journal of Aeronautics. 2018;31(3):556-66.##
[11] Zhao X, Li J, Yan X, Ji S. Robust adaptive cubature Kalman filter and its application to ultra-tightly coupled SINS/GPS navigation system. Sensors. 2018;18(7):2352.##
[12] Chiang K-W, Tsai G-J, Chang H, Joly C, Ei-Sheimy N. Seamless navigation and mapping using an INS/GNSS/grid-based SLAM semi-tightly coupled integration scheme. Information Fusion. 2019;50:181-96.##
[13] Zhang P, Hancock CM, Lau L, Roberts GW, de Ligt H. Low-cost IMU and odometer tightly coupled integration with Robust Kalman filter for underground 3-D pipeline mapping. Measurement. 2019;137:454-63.##
[14] Xie F, Sun R, Kang G, Qian W, Zhao J, Zhang L. A jamming tolerant BeiDou combined B1/B2 vector tracking algorithm for ultra-tightly coupled GNSS/INS systems. Aerospace Science and Technology. 2017;70:265-76.##
[15] Gao Z, Ge M, Shen W, Li Y, Chen Q, Zhang H, et al. Evaluation on the impact of IMU grades on BDS+ GPS PPP/INS tightly coupled integration. Advances in Space Research. 2017;60(6):1283-99.##
[16] Nguyen H-D, Nguyen V-H, Nguyen H-V, editors. Tightly-coupled INS/GPS integration with magnetic aid. 2017 2nd International Conference on Control and Robotics Engineering (ICCRE); 2017: IEEE.##
[17] Li Z, Chang G, Gao J, Wang J, Hernandez A. GPS/UWB/MEMS-IMU tightly coupled navigation with improved robust Kalman filter. Advances in Space Research. 2016;58(11):2424-34.##
[18] Tseng C-H, Lin S-F, Jwo D-J. Fuzzy adaptive cubature Kalman filter for integrated navigation systems. Sensors. 2016;16(8):1167.##
[19] A. Ramezani JZPD, and M. S. Ph.D. Performance improvement of the inertial navigation system using unscented and cubature Kalman filters. Shiraz Univ Technol. 2013.##
[20] Nazemipour A, Manzuri MT, Kamran D, Karimian M. MEMS gyro bias estimation in accelerated motions using sensor fusion of camera and angular-rate gyroscope. IEEE Transactions on Vehicular Technology. 2020;69(4):3841-51.##
[21] M. Alinezhad DHK, and Dr. Gholamreza Akbarizadeh. Design and construction inertial navigation system. Shahid Chamran Univ Ahvaz,. 2015.##
[22] N. Moazzen DHK, and D. K. Ansari. Navigation Accuracy Enhancement of Integrated GPS/INS System using Nonlinear SDRE Filtering. Shahid Chamran Univ Ahvaz,. 2016.##
[23] M. M. H. Darani DHN, and D. H. G. Asl. Nonlinear Filters Applied to Tightly Coupled Integration of INS/GPS/PL for Precise Navigation in Automatic Landing of UAVs. Sharif Univ Technol. 2015.##
[24] Ren J, Zi J, Guan H, Li J, editors. Design of an Ultra-Tightly Coupled Integrated INS/GPS Navigation System Based on UPF. 2020 27th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS); 2020: IEEE.##
[25] Gao B, Hu G, Zhong Y, Zhu X. Cubature Kalman filter with both adaptability and robustness for tightly-coupled GNSS/INS integration. IEEE Sensors Journal. 2021;21(13):14997-5011.##
[26] Zhang J, Zhang T, Jiang X, Wang S, editors. Tightly coupled GPS/INS integrated navigation algorithm based on Kalman filter. 2012 Second International Conference on Business Computing and Global Informatization; 2012: IEEE.##
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