A stellar/inertial integrated navigation method based on the observation of the star centroid prediction error-Reference-Cited by-同舟云学术

A stellar/inertial integrated navigation method based on the observation of the star centroid prediction error

Published:2021-03-01 Issue:3 Volume:92 Page:035001
ISSN:0034-6748
Container-title:Review of Scientific Instruments
language:en
Short-container-title:Review of Scientific Instruments

Author:

Ni Yuanman¹^ORCID,Tan Wenfeng¹^ORCID,Dai Dongkai¹,Wang Xingshu¹,Qin Shiqiao¹^ORCID

Affiliation:

1. College of Advanced Interdisciplinary Studies, National University of Defense Technology, Changsha 410073, Hunan, China

Funder

National Natural Science Foundation of China

Natural Science Foundation of Hunan Province

Publisher

AIP Publishing

Subject

Instrumentation

Link

https://aip.scitation.org/doi/pdf/10.1063/5.0027530

Reference24 articles.

1. O. J. Woodman, “An introduction to inertial navigation,” Technical Report No. UCAMCL-TR-696, Computer Laboratory, University of Cambridge, Cambridge, UK, August 2007.

2. An approach to benchmarking of loosely coupled low-cost navigation systems

3. Alternatives to GPS

4. Three-axis attitude accuracy of better than 5 arcseconds obtained for the star sensor in a long-term on-ship dynamic experiment

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. An Evaluation Model of Star Sensor Observation Capability Under Hypersonic Aerothermal Conditions;IEEE Access;2023

2. LSTM-Based Shuler Oscillation Error Restriction for Shipborne SINS;Lecture Notes in Electrical Engineering;2023

3. Research on joint calibration and compensation of the inclinometer installation and instrument errors in the celestial positioning system;Journal of Field Robotics;2022-06-20

4. Self-calibration of cameras using affine correspondences and known relative rotation angle;Applied Optics;2021-12-02