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2020 – today
- 2023
[j22]Lubin Chang
, Yarong Luo:
Log-Linear Error State Model Derivation Without Approximation for INS. IEEE Trans. Aerosp. Electron. Syst. 59(2): 2029-2035 (2023)- [j21]Lubin Chang, Hongqiong Tang, Gaoge Hu, Jiangning Xu:
SINS/DVL Linear Initial Alignment Based on Lie Group SE3(3). IEEE Trans. Aerosp. Electron. Syst. 59(5): 7203-7217 (2023) - [j20]Gaoge Hu, Linyan Xu, Bingbing Gao, Lubin Chang, Yongmin Zhong:
Robust Unscented Kalman Filter-Based Decentralized Multisensor Information Fusion for INS/GNSS/CNS Integration in Hypersonic Vehicle Navigation. IEEE Trans. Instrum. Meas. 72: 1-11 (2023) - [j19]Hongqiong Tang, Jiangning Xu, Lubin Chang, Wence Shi, Hongyang He:
Invariant Error-Based Integrated Solution for SINS/DVL in Earth Frame: Extension and Comparison. IEEE Trans. Instrum. Meas. 72: 1-17 (2023) - 2022
- [j18]Jiupeng Zhu, An Li, Fangjun Qin, Lubin Chang:
A New Robust Adaptive Filter Aided by Machine Learning Method for SINS/DVL Integrated Navigation System. Sensors 22(10): 3792 (2022) - [j17]Xu Lyu, Baiqing Hu, Zheng Wang, Duanyang Gao, Kailong Li, Lubin Chang:
A SINS/GNSS/VDM Integrated Navigation Fault-Tolerant Mechanism Based on Adaptive Information Sharing Factor. IEEE Trans. Instrum. Meas. 71: 1-13 (2022) - [i11]Lubin Chang, Yarong Luo:
Log-linear Error State Model Derivation without Approximation for INS. CoRR abs/2208.03427 (2022) - 2021
- [j16]Duanyang Gao, Baiqing Hu, Lubin Chang, Fangjun Qin, Xu Lyu:
An Aided Navigation Method Based on Strapdown Gravity Gradiometer. Sensors 21(3): 829 (2021) - [i10]Lubin Chang, Fangjun Qin, Jiangning Xu:
Strapdown Inertial Navigation System Initial Alignment based on Group of Double Direct Spatial Isometries. CoRR abs/2102.12697 (2021) - [i9]Lubin Chang, Jingbo Di, Fangjun Qin:
Inertial based Integration with Transformed INS Mechanization in Earth Frame. CoRR abs/2103.02229 (2021) - [i8]Lubin Chang:
MEKF Ignoring Initial Conditions for Attitude Estimation Using Vector Observations. CoRR abs/2110.13666 (2021) - 2020
- [i7]Lubin Chang:
SE(3) based Extended Kalman Filter for Spacecraft Attitude Estimation. CoRR abs/2003.12978 (2020)
2010 – 2019
- 2019
- [j15]Lubin Chang, Fangjun Qin, Meiping Wu:
Gravity Disturbance Compensation for Inertial Navigation System. IEEE Trans. Instrum. Meas. 68(10): 3751-3765 (2019) - 2018
- [j14]Bing Zhu, Lubin Chang, Jiangning Xu, Feng Zha, Jingshu Li:
Huber-Based Adaptive Unscented Kalman Filter with Non-Gaussian Measurement Noise. Circuits Syst. Signal Process. 37(9): 3842-3861 (2018) - [j13]Junbo Tie, Juliang Cao, Lubin Chang, Shaokun Cai, Meiping Wu, Junxiang Lian:
A Model of Gravity Vector Measurement Noise for Estimating Accelerometer Bias in Gravity Disturbance Compensation. Sensors 18(3): 883 (2018) - [j12]Fangjun Qin, Lubin Chang, Sai Jiang, Feng Zha:
A Sequential Multiplicative Extended Kalman Filter for Attitude Estimation Using Vector Observations. Sensors 18(5): 1414 (2018) - [i6]Lubin Chang:
Semi-Analytic Method for SINS Attitude and Parameters Online Estimation. CoRR abs/1801.05212 (2018) - 2017
- [j11]Lubin Chang, Kailong Li:
Unified Form for the Robust Gaussian Information Filtering Based on M-Estimate. IEEE Signal Process. Lett. 24(4): 412-416 (2017) - [j10]Jiangning Xu, Hongyang He, Fangjun Qin, Lubin Chang:
A Novel Autonomous Initial Alignment Method for Strapdown Inertial Navigation System. IEEE Trans. Instrum. Meas. 66(9): 2274-2282 (2017) - [c2]Baiqing Hu, Lubin Chang, Fangjun Qin:
Robust Gaussian filtering based on M-estimate with adaptive measurement noise covariance. FUSION 2017: 1-6 - [c1]Fangjun Qin, Lubin Chang:
Velocity integration of strapdown inertial navigation using modified unscented quaternion estimator. FUSION 2017: 1-6 - [i5]Lubin Chang, Fangjun Qin:
Dynamic Analytical Initialization Method for Spacecraft Attitude Estimators. CoRR abs/1706.06814 (2017) - [i4]Lubin Chang:
Alternate Derivation of Geometric Extended Kalman Filter by MEKF Approach. CoRR abs/1710.03949 (2017) - 2016
- [j9]Lubin Chang, Jingshu Li, Kailong Li:
Optimization-based alignment for strapdown inertial navigation system: comparison and extension. IEEE Trans. Aerosp. Electron. Syst. 52(4): 1697-1713 (2016) - [j8]Lubin Chang, Baiqing Hu, Kailong Li:
Iterated multiplicative extended kalman filter for attitude estimation using vector observations. IEEE Trans. Aerosp. Electron. Syst. 52(4): 2053-2060 (2016) - 2015
- [j7]Lubin Chang, Fangjun Qin, An Li:
A Novel Backtracking Scheme for Attitude Determination-Based Initial Alignment. IEEE Trans Autom. Sci. Eng. 12(1): 384-390 (2015) - [j6]Lubin Chang, Jingshu Li, Shengyong Chen:
Initial Alignment by Attitude Estimation for Strapdown Inertial Navigation Systems. IEEE Trans. Instrum. Meas. 64(3): 784-794 (2015) - [j5]Lubin Chang, Baiqing Hu, Yang Li:
Backtracking Integration for Fast Attitude Determination-Based Initial Alignment. IEEE Trans. Instrum. Meas. 64(3): 795-803 (2015) - [j4]Kailong Li, Lubin Chang, Baiqing Hu:
Unscented Attitude Estimator Based on Dual Attitude Representations. IEEE Trans. Instrum. Meas. 64(12): 3564-3576 (2015) - [i3]Lubin Chang:
On Kalman-Like Finite Impulse Response Filters. CoRR abs/1501.07132 (2015) - 2014
- [i2]Lubin Chang, Baiqing Hu, Jingshu Li, Kailong Li:
Optimization-based Alignment for Strapdown Inertial Navigation System Comparison and Extension. CoRR abs/1411.5869 (2014) - [i1]Lubin Chang:
Particle Filtering for Attitude Estimation Using a Minimal Local-Error Representation: A Revisit. CoRR abs/1411.6127 (2014) - 2013
- [j3]Lubin Chang, Baiqing Hu, An Li, Fangjun Qin:
Unscented type Kalman filter: limitation and combination. IET Signal Process. 7(3): 167-176 (2013) - [j2]Lubin Chang, Baiqing Hu, An Li, Fangjun Qin:
Transformed Unscented Kalman Filter. IEEE Trans. Autom. Control. 58(1): 252-257 (2013) - [j1]Lubin Chang, Baiqing Hu, Shengyong Chen, Fangjun Qin:
Comments on "Quaternion-Based Method for SINS/SAR Integrated Navigation System". IEEE Trans. Aerosp. Electron. Syst. 49(2): 1400-1402 (2013)
Coauthor Index
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