Jie Li
Orcid: 0000-0001-6873-7648Affiliations:
- North University of China, Key Laboratory of Instrumentation Science & Dynamic Measurement / China National Key Laboratory for Electronic Measurement Technology, Taiyuan, China
- Beijing Institute of Technology, Department of Automatic Control, China (PhD 2005)
According to our database1,
Jie Li
authored at least 30 papers
between 2016 and 2023.
Collaborative distances:
Collaborative distances:
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Bibliography
2023
An In-Flight Alignment Method for Global Positioning System-Assisted Low Cost Strapdown Inertial Navigation System in Flight Body with Short-Endurance and High-Speed Rotation.
Remote. Sens., February, 2023
Robust Adaptive Heading Tracking Fusion for Polarization Compass With Uncertain Dynamics and External Disturbances.
IEEE Trans. Instrum. Meas., 2023
2022
Optimal Rotational Angular Velocity Determination Method Based on Compound Rotary Semi-Strapdown Inertial Navigation System.
Sensors, 2022
Improved Multiple-Model Adaptive Estimation Method for Integrated Navigation with Time-Varying Noise.
Sensors, 2022
Sensors, 2022
Sensors, 2022
An Improved In-flight Alignment Method Based on Backtracking Navigation for GPS-aided Low Cost SINS With Short Endurance.
IEEE Robotics Autom. Lett., 2022
Sci. China Inf. Sci., 2022
2021
Seamless GPS/Inertial Navigation System Based on Self-Learning Square-Root Cubature Kalman Filter.
IEEE Trans. Ind. Electron., 2021
Frontiers Inf. Technol. Electron. Eng., 2021
Research on the Update Method of Attitude Quaternion for Strapdown Inertial Navigation.
IEEE Access, 2021
A Mixed Optimization Method Based on Adaptive Kalman Filter and Wavelet Neural Network for INS/GPS During GPS Outages.
IEEE Access, 2021
Robust Central Difference Kalman Filter With Mixture Correntropy: A Case Study for Integrated Navigation.
IEEE Access, 2021
Robust Cubature Kalman Filter for SINS/GPS Integrated Navigation Systems With Unknown Noise Statistics.
IEEE Access, 2021
AGMC-Based Robust Cubature Kalman Filter for SINS/GNSS Integrated Navigation System With Unknown Noise Statistics.
IEEE Access, 2021
2020
A New In-Flight Alignment Method with an Application to the Low-Cost SINS/GPS Integrated Navigation System.
Sensors, 2020
Optimal Design and Analysis on High Overload Buffer Structure of Passive Semi-Strapdown Inertial Navigation System.
Sensors, 2020
IEEE Access, 2020
2019
Sensors, 2019
A Novel Rotation Scheme for MEMS IMU Error Mitigation Based on a Missile-Borne Rotation Semi-Strapdown Inertial Navigation System.
Sensors, 2019
Delay-Free Tracking Differentiator Design Based on Variational Mode Decomposition: Application on MEMS Gyroscope Denoising.
J. Sensors, 2019
IEEE Access, 2019
Analysis and Compensation of Installation Errors for Rotating Semi-Strapdown Inertial Navigation System.
IEEE Access, 2019
Optimized Design of an Anti-Rotation and Anti-Overload Structure Based on Missile-Borne Semi-Strap-Down Inertial Navigation System.
IEEE Access, 2019
2018
Analysis and Compensation of Modulation Angular Rate Error Based on Missile-Borne Rotation Semi-Strapdown Inertial Navigation System.
Sensors, 2018
An Improved Strong Tracking Cubature Kalman Filter for GPS/INS Integrated Navigation Systems.
Sensors, 2018
2017
Correction: A New Quaternion-Based Kalman Filter for Real-Time Attitude Estimation Using the Two-Step Geometrically-Intuitive Correction Algorithm. <i>Sensors</i> 2017, <i>17</i>, 2146.
Sensors, 2017
A New Quaternion-Based Kalman Filter for Real-Time Attitude Estimation Using the Two-Step Geometrically-Intuitive Correction Algorithm.
Sensors, 2017
2016
A Noise Reduction Method for Dual-Mass Micro-Electromechanical Gyroscopes Based on Sample Entropy Empirical Mode Decomposition and Time-Frequency Peak Filtering.
Sensors, 2016