桂明臻｜中南大学｜学者主页

2025

基于QLUKF的深空探测器测角/星光相对论扰动组合导航方法

桂明臻，林绍辉，叶文，魏一丰，薛晓鹏

《中南大学学报(自然科学版)》

2025

一种木星探测器天文测角/相对论组合导航方法

桂明臻，张展赫，熊凯，宁晓琳

《深空探测学报(中英文)》

DOI

2025

Advances in Deep Space Probe Navigation

Mingzhen Gui, Jin Liu, Cheng-Xi Zhang, Ming-Zhe Dai

Applied Sciences

DOI

2024

基于GPR-UKF的天文测角/测速组合导航方法

张寿健，桂明臻

《系统工程与电子技术》

2024

Time Dilation Modified-TDTOA/StarNAV Integrated Navigation Method for Mars Exploration

Mingzhen Gui, Yifeng Wei, Xiao-Lin Ning, Xing Li

IEEE Transactions on Instrumentation and Measurement

DOI

2024

Star Angle Modified with Relativistic Effects/StarNAV Integrated Navigation Method for Mars Exploration

Mingzhen Gui, Yifeng Wei, Hua Yang, Yu-Qing Yang

Advances in Space Research

DOI

2024

Anelosimus eximius Colony Algorithm and Its Application to Celestial Doppler Difference Velocimetry

Zhou-qian Xiang, Jin Liu, Mingzhen Gui, Z. Kang, Dian Jin

Journal of Aerospace Engineering

DOI

2023

考虑相对论效应的火星探测器天文测角导航

桂明臻，魏一丰，宁晓琳

《深空探测学报(中英文)》

2023

Analysis and Compensation of Sun Direction Error on Solar Disk Velocity Difference

Mingzhen Gui, Hua Yang, Dang-Jun Zhao, Ming-Zhe Dai, Cheng-Xi Zhang

Mathematics

DOI

2023

Parameter-Independent Event-Triggered Implicit UKF for the Celestial Navigation Using Time Delay Measurement

Mingzhen Gui, Cai-Sheng Wei, Yifeng Wei, K. Xiong, Cheng-Xi Zhang, Ming-Zhe Dai

Mathematics

DOI

2023

A Novel Sun Direction/Solar Disk Velocity Difference Integrated Navigation Method Against Installation Error of Spectrometer Array

Mingzhen Gui, Hua Yang, Xiaolin Ning, Wen Ye, Caisheng Wei

IEEE Sensors Journal

DOI

2022

Variational Bayesian implicit unscented Kalman filter for celestial navigation using time delay measurement

Mingzhen Gui, Hua Yang, Xiaolin Ning, Da Zhao, Linzhouting Chen, Ming-Zhe Dai

Advances in Space Research

DOI

2022

Star Angle/ Double-Differenced Pulse Time of Arrival Integrated Navigation Method for Jupiter exploration

Mingzhen Gui, Hua Yang, X. Ning, Kai Xiong, Jin Liu, Ming-Zhe Dai

Advances in Space Research

DOI

2021

基于TOA和TDTOA的增广状态脉冲星组合导航误差抑制方法

宁晓琳，桂明臻，黄月清，房建成，吴伟仁

《中国科学:信息科学》

2021

一种快速星光角距/时间延迟量测组合导航方法

桂明臻，宁晓琳，马辛，叶文

《深空探测学报(中英文)》

DOI

2021

A Time Delay/Star Angle Integrated Navigation Method Based on the Event-Triggered Implicit Unscented Kalman Filter

Mingzhen Gui, Dang-Jun Zhao, Xiaolin Ning, Cheng-Xi Zhang, Ming-Zhe Dai

IEEE Transactions on Instrumentation and Measurement

DOI

2020

考虑星历误差的天文测角/时间延迟量测组合导航方法

桂明臻，宁晓琳，芦佳振，魏才盛

《飞控与探测》

DOI

2019

一种基于太阳震荡时间延迟量测的自主天文导航方法

宁晓琳，桂明臻，孙晓函，刘劲，吴伟仁

《深空探测学报(中英文)》

DOI

2019

High-accuracy pulsar time delay estimation using an FrFT-based GCC

Y. Rao, Z. Kang, Jin Liu, Xin Ma, Mingzhen Gui

Optik (Stuttgart)

DOI

2019

A Novel Celestial Aided Time-Differenced Pulsar Navigation Method Against Ephemeris Error of Jupiter for Jupiter Exploration

Mingzhen Gui, Xiaolin Ning, Xin Ma, Jie Zhang

IEEE Sensors Journal

DOI

2018

深空探测器自主天文导航技术综述

房建成，宁晓琳，马辛，刘劲，桂明臻

《飞控与探测》

2018

面向编队飞行的天文多普勒差分/脉冲星组合导航

喻子原，刘劲，宁晓琳，马辛，桂明臻，康志伟

《深空探测学报(中英文)》

2018

A Novel Autonomous Celestial Navigation Method Using Solar Oscillation Time Delay Measurement

Xiaolin Ning, Mingzhen Gui, Jian-Cheng Fang, Gang Liu, Weiren Wu

IEEE Transactions on Aerospace and Electronic Systems

DOI

2018

Ephemeris Corrections in Celestial/Pulsar Navigation Using Time Differential and Ephemeris Estimation

Xiaolin Ning, Yuqing Yang, Zhuo Li, Mingzhen Gui, Jian-Cheng Fang

DOI

2018

A Fast Calibration Method of the Star Sensor Installation Error Based on Observability Analysis for the Tightly Coupled SINS/CNS-Integrated Navigation System

Xiaolin Ning, Jie Zhang, Mingzhen Gui, Jian-Cheng Fang

IEEE Sensors Journal

DOI

2018

Pulsar navigation using time of arrival (TOA) and time differential TOA (TDTOA)

Xiaolin Ning, Yuqing Yang, Mingzhen Gui, Weiren Wu, Jian-Cheng Fang, Gang Liu

DOI

2018

Adaptive pulsar time delay estimation using wavelet-based RLS

Z. Kang, Hongcai He, Jin Liu, Xin Ma, Mingzhen Gui

Optik (Stuttgart)

DOI

2018

Pulsar time delay estimation method based on two-level compressed sensing

Z. Kang, Chun-Yan Wu, Jin Liu, Xin Ma, Mingzhen Gui

DOI

2017

Initial Attitude Estimation and Installation Errors Calibration of the IMU for Plane by SINS/CNS Integration

Weiping Yuan, Mingzhen Gui, Xiaolin Ning

DOI

2017

A Novel Differential Doppler Measurement-Aided Autonomous Celestial Navigation Method for Spacecraft During Approach Phase

Xiaolin Ning, Mingzhen Gui, Jian-Cheng Fang, Yu Dai, Gang Liu

IEEE Transactions on Aerospace and Electronic Systems

DOI

2017

Impact of the Pulsar‘s Direction on CNS/XNAV Integrated Navigation

Xiaolin Ning, Mingzhen Gui, Jie Zhang, Jian-Cheng Fang, Gang Liu

IEEE Transactions on Aerospace and Electronic Systems

DOI

2017

Solar oscillation time delay measurement assisted celestial navigation method

Xiaolin Ning, Mingzhen Gui, Jie Zhang, Jian-Cheng Fang, Gang Liu

DOI

2017

Differential X-ray pulsar aided celestial navigation for Mars exploration

Xiaolin Ning, Mingzhen Gui, Jian-Cheng Fang, Gang Liu

DOI

2017

Structured condition number and its application in celestial navigation system with variable observability degree

J. Liu, Xiaolin Ning, Xin Ma, Mingzhen Gui, Jian-Cheng Fang, Gang Liu

DOI

2016

INS/VNS/CNS integrated navigation method for planetary rovers

Xiaolin Ning, Mingzhen Gui, Yong-Zhi Xu, Xin-Bei Bai, Jian-Cheng Fang

DOI

2016

A dimension reduced INS/VNS integrated navigation method for planetary rovers

Xiaolin Ning, Mingzhen Gui, Jie Zhang, Jian-Cheng Fang

DOI

2016

次元は惑星ローバのためのINS/VNS統合航法を減少させた【Powered by NICT】

Xiaolin Ning, Mingzhen Gui, Jie Zhang, Jian-Cheng Fang

精选作品

期刊论文

基于QLUKF的深空探测器测角/星光相对论扰动组合导航方法

一种木星探测器天文测角/相对论组合导航方法

Advances in Deep Space Probe Navigation

基于GPR-UKF的天文测角/测速组合导航方法

Time Dilation Modified-TDTOA/StarNAV Integrated Navigation Method for Mars Exploration

Star Angle Modified with Relativistic Effects/StarNAV Integrated Navigation Method for Mars Exploration

Anelosimus eximius Colony Algorithm and Its Application to Celestial Doppler Difference Velocimetry

考虑相对论效应的火星探测器天文测角导航

Analysis and Compensation of Sun Direction Error on Solar Disk Velocity Difference

Parameter-Independent Event-Triggered Implicit UKF for the Celestial Navigation Using Time Delay Measurement

A Novel Sun Direction/Solar Disk Velocity Difference Integrated Navigation Method Against Installation Error of Spectrometer Array

Variational Bayesian implicit unscented Kalman filter for celestial navigation using time delay measurement

Star Angle/ Double-Differenced Pulse Time of Arrival Integrated Navigation Method for Jupiter exploration

基于TOA和TDTOA的增广状态脉冲星组合导航误差抑制方法

一种快速星光角距/时间延迟量测组合导航方法

A Time Delay/Star Angle Integrated Navigation Method Based on the Event-Triggered Implicit Unscented Kalman Filter

考虑星历误差的天文测角/时间延迟量测组合导航方法

一种基于太阳震荡时间延迟量测的自主天文导航方法

High-accuracy pulsar time delay estimation using an FrFT-based GCC

A Novel Celestial Aided Time-Differenced Pulsar Navigation Method Against Ephemeris Error of Jupiter for Jupiter Exploration

深空探测器自主天文导航技术综述

面向编队飞行的天文多普勒差分/脉冲星组合导航

A Novel Autonomous Celestial Navigation Method Using Solar Oscillation Time Delay Measurement

Ephemeris Corrections in Celestial/Pulsar Navigation Using Time Differential and Ephemeris Estimation

A Fast Calibration Method of the Star Sensor Installation Error Based on Observability Analysis for the Tightly Coupled SINS/CNS-Integrated Navigation System

Pulsar navigation using time of arrival (TOA) and time differential TOA (TDTOA)

Adaptive pulsar time delay estimation using wavelet-based RLS

Pulsar time delay estimation method based on two-level compressed sensing

Initial Attitude Estimation and Installation Errors Calibration of the IMU for Plane by SINS/CNS Integration

A Novel Differential Doppler Measurement-Aided Autonomous Celestial Navigation Method for Spacecraft During Approach Phase

Impact of the Pulsar‘s Direction on CNS/XNAV Integrated Navigation

Solar oscillation time delay measurement assisted celestial navigation method

Differential X-ray pulsar aided celestial navigation for Mars exploration

Structured condition number and its application in celestial navigation system with variable observability degree

INS/VNS/CNS integrated navigation method for planetary rovers

A dimension reduced INS/VNS integrated navigation method for planetary rovers

次元は惑星ローバのためのINS/VNS統合航法を減少させた【Powered by NICT】

会议论文

Attitude Estimation Method for Spinning Spacecraft Using Markley Variables and Optical Flow of Stars

书籍章节

Birkhoff Pseudospectral Method and Convex Programming for Trajectory Optimization

研究方向