Kaiqiang Feng

Orcid: 0000-0002-8080-6025

According to our database¹, Kaiqiang Feng authored at least 25 papers between 2017 and 2023.

Collaborative distances:

Dijkstra number² of four.
Erdős number³ of four.

Timeline

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On csauthors.net:

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.

[BibT_eX]

[DOI]

Remote. Sens., February, 2023

Decoding of the neural representation of the visual RGB color model.

[BibT_eX]

[DOI]

PeerJ Comput. Sci., 2023

2022

Optimal Rotational Angular Velocity Determination Method Based on Compound Rotary Semi-Strapdown Inertial Navigation System.

[BibT_eX]

[DOI]

Sensors, 2022

An Anti-Turbulence Self-Alignment Method for SINS under Unknown Latitude Conditions.

[BibT_eX]

[DOI]

Sensors, 2022

An Improved In-flight Alignment Method Based on Backtracking Navigation for GPS-aided Low Cost SINS With Short Endurance.

[BibT_eX]

[DOI]

IEEE Robotics Autom. Lett., 2022

2021

A Low-Cost MEMS Missile-Borne Compound Rotation Modulation Scheme.

[BibT_eX]

[DOI]

Sensors, 2021

A BCH error correction scheme applied to FPGA with embedded memory.

[BibT_eX]

[DOI]

Frontiers Inf. Technol. Electron. Eng., 2021

Research on the Update Method of Attitude Quaternion for Strapdown Inertial Navigation.

[BibT_eX]

[DOI]

IEEE Access, 2021

A Mixed Optimization Method Based on Adaptive Kalman Filter and Wavelet Neural Network for INS/GPS During GPS Outages.

[BibT_eX]

[DOI]

IEEE Access, 2021

Robust Central Difference Kalman Filter With Mixture Correntropy: A Case Study for Integrated Navigation.

[BibT_eX]

[DOI]

IEEE Access, 2021

Robust Cubature Kalman Filter for SINS/GPS Integrated Navigation Systems With Unknown Noise Statistics.

[BibT_eX]

[DOI]

IEEE Access, 2021

AGMC-Based Robust Cubature Kalman Filter for SINS/GNSS Integrated Navigation System With Unknown Noise Statistics.

[BibT_eX]

[DOI]

IEEE Access, 2021

2020

A New In-Flight Alignment Method with an Application to the Low-Cost SINS/GPS Integrated Navigation System.

[BibT_eX]

[DOI]

Sensors, 2020

Research on Dynamic Test of Hyper-Velocity Impact Penetration Acceleration Signal.

[BibT_eX]

[DOI]

IEEE Access, 2020

Influence of Magnetically Confined Plasma on the Muzzle Velocity of Gun Projectile.

[BibT_eX]

[DOI]

IEEE Access, 2020

2019

Optimization of a New High Rotary Missile-Borne Stabilization Platform.

[BibT_eX]

[DOI]

Sensors, 2019

A Novel Rotation Scheme for MEMS IMU Error Mitigation Based on a Missile-Borne Rotation Semi-Strapdown Inertial Navigation System.

[BibT_eX]

[DOI]

Sensors, 2019

Signal Measurement of Projectile Penetration Overload Based on Charge Sensor.

[BibT_eX]

[DOI]

IEEE Access, 2019

Analysis and Compensation of Installation Errors for Rotating Semi-Strapdown Inertial Navigation System.

[BibT_eX]

[DOI]

IEEE Access, 2019

Optimized Design of an Anti-Rotation and Anti-Overload Structure Based on Missile-Borne Semi-Strap-Down Inertial Navigation System.

[BibT_eX]

[DOI]

IEEE Access, 2019

Face Recognition in Complex Lighting Environment.

[BibT_eX]

[DOI]

Proceedings of the 2019 International Conference on Cyber-Enabled Distributed Computing and Knowledge Discovery, 2019

2018

Analysis and Compensation of Modulation Angular Rate Error Based on Missile-Borne Rotation Semi-Strapdown Inertial Navigation System.

[BibT_eX]

[DOI]

Sensors, 2018

An Improved Strong Tracking Cubature Kalman Filter for GPS/INS Integrated Navigation Systems.

[BibT_eX]

[DOI]

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.

[BibT_eX]

[DOI]

Sensors, 2017

A New Quaternion-Based Kalman Filter for Real-Time Attitude Estimation Using the Two-Step Geometrically-Intuitive Correction Algorithm.

[BibT_eX]