Spoofing Control Strategy for Precise Position Offset Based on INS/GNSS Tightly Coupled Navigation

To deceive Inertial Navigation System(INS)/Global Navigation Satellite System(GNSS) integrated navigation terminals, the entry point is still to inject GNSS spoofing signals to the target system. However, the spoofing control strategy in integrated navigation mode for particular tasks such as fixed-...

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Main Authors: Shuhai Lu, Yan Guo, Hang Shang, Kanghua Tang, Juliang Cao, Ruihang Yu, Shaokun Cai
Format: Article
Language:English
Published: IEEE 2020-01-01
Series:IEEE Access
Subjects:
Online Access:https://ieeexplore.ieee.org/document/9104955/
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spelling doaj-f5bda60fcc724814a48e0ba6858a55ac2021-03-30T02:14:27ZengIEEEIEEE Access2169-35362020-01-01810358510360010.1109/ACCESS.2020.29990869104955Spoofing Control Strategy for Precise Position Offset Based on INS/GNSS Tightly Coupled NavigationShuhai Lu0https://orcid.org/0000-0002-1454-8443Yan Guo1https://orcid.org/0000-0002-2483-5526Hang Shang2https://orcid.org/0000-0002-0729-4588Kanghua Tang3Juliang Cao4https://orcid.org/0000-0003-4704-4919Ruihang Yu5https://orcid.org/0000-0003-4258-908XShaokun Cai6College of Intelligence Science and Technology, National University of Defence Technology, Changsha, ChinaCollege of Intelligence Science and Technology, National University of Defence Technology, Changsha, ChinaCollege of Intelligence Science and Technology, National University of Defence Technology, Changsha, ChinaCollege of Intelligence Science and Technology, National University of Defence Technology, Changsha, ChinaCollege of Intelligence Science and Technology, National University of Defence Technology, Changsha, ChinaCollege of Intelligence Science and Technology, National University of Defence Technology, Changsha, ChinaCollege of Intelligence Science and Technology, National University of Defence Technology, Changsha, ChinaTo deceive Inertial Navigation System(INS)/Global Navigation Satellite System(GNSS) integrated navigation terminals, the entry point is still to inject GNSS spoofing signals to the target system. However, the spoofing control strategy in integrated navigation mode for particular tasks such as fixed-point capture or directional drive needs further research. Whether applying GNSS spoofing attacks or not, the Kalman filter correction gain matrix element in the tightly coupled navigation system always maintains its stability, which gives us valuable clues to develop an effective spoofing attack. On this basis, this article focuses on the feasibility and operability of spoofing attacks under tightly coupled navigation conditions and innovatively proposes a spoofing control strategy that can achieve accurate position offsets: Specific spoofing signals are implanted to the target tightly coupled navigation terminal at the beginning of the spoofing attack. The amounts of pseudo-range spoofing signals corresponding to different satellites are respectively the projections of the position increments to be deceived on the sight vector of the integrated navigation terminal to each satellite. Simulation experiments and tightly coupled navigation terminal experiments verify the correctness and effectiveness of the spoofing control strategy.https://ieeexplore.ieee.org/document/9104955/INS/GNSS tightly coupled navigationspoofing control strategysteady state gain matrixGNSS spoofing signalprecise position offset
collection DOAJ
language English
format Article
sources DOAJ
author Shuhai Lu
Yan Guo
Hang Shang
Kanghua Tang
Juliang Cao
Ruihang Yu
Shaokun Cai
spellingShingle Shuhai Lu
Yan Guo
Hang Shang
Kanghua Tang
Juliang Cao
Ruihang Yu
Shaokun Cai
Spoofing Control Strategy for Precise Position Offset Based on INS/GNSS Tightly Coupled Navigation
IEEE Access
INS/GNSS tightly coupled navigation
spoofing control strategy
steady state gain matrix
GNSS spoofing signal
precise position offset
author_facet Shuhai Lu
Yan Guo
Hang Shang
Kanghua Tang
Juliang Cao
Ruihang Yu
Shaokun Cai
author_sort Shuhai Lu
title Spoofing Control Strategy for Precise Position Offset Based on INS/GNSS Tightly Coupled Navigation
title_short Spoofing Control Strategy for Precise Position Offset Based on INS/GNSS Tightly Coupled Navigation
title_full Spoofing Control Strategy for Precise Position Offset Based on INS/GNSS Tightly Coupled Navigation
title_fullStr Spoofing Control Strategy for Precise Position Offset Based on INS/GNSS Tightly Coupled Navigation
title_full_unstemmed Spoofing Control Strategy for Precise Position Offset Based on INS/GNSS Tightly Coupled Navigation
title_sort spoofing control strategy for precise position offset based on ins/gnss tightly coupled navigation
publisher IEEE
series IEEE Access
issn 2169-3536
publishDate 2020-01-01
description To deceive Inertial Navigation System(INS)/Global Navigation Satellite System(GNSS) integrated navigation terminals, the entry point is still to inject GNSS spoofing signals to the target system. However, the spoofing control strategy in integrated navigation mode for particular tasks such as fixed-point capture or directional drive needs further research. Whether applying GNSS spoofing attacks or not, the Kalman filter correction gain matrix element in the tightly coupled navigation system always maintains its stability, which gives us valuable clues to develop an effective spoofing attack. On this basis, this article focuses on the feasibility and operability of spoofing attacks under tightly coupled navigation conditions and innovatively proposes a spoofing control strategy that can achieve accurate position offsets: Specific spoofing signals are implanted to the target tightly coupled navigation terminal at the beginning of the spoofing attack. The amounts of pseudo-range spoofing signals corresponding to different satellites are respectively the projections of the position increments to be deceived on the sight vector of the integrated navigation terminal to each satellite. Simulation experiments and tightly coupled navigation terminal experiments verify the correctness and effectiveness of the spoofing control strategy.
topic INS/GNSS tightly coupled navigation
spoofing control strategy
steady state gain matrix
GNSS spoofing signal
precise position offset
url https://ieeexplore.ieee.org/document/9104955/
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