The Simulation of ICCP Algorithm in the Gravity Aided Navigation

It is well known that the position errors of INS are accumulated with the time. In order to achieve high accuracy navigation, the vehicle must have other aided navigation methods. The process of receive signals such as GPS destroys the task of the under vehicle. The passive navigation system based o...

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Published in2009 Second International Conference on Intelligent Networks and Intelligent Systems pp. 62 - 65
Main Authors Yi, Cheng, Buo, Xiu Chun, Jing, Luo
Format Conference Proceeding
LanguageEnglish
Published IEEE 01.11.2009
Subjects
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ISBN142445557X
9781424455577
DOI10.1109/ICINIS.2009.25

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Abstract It is well known that the position errors of INS are accumulated with the time. In order to achieve high accuracy navigation, the vehicle must have other aided navigation methods. The process of receive signals such as GPS destroys the task of the under vehicle. The passive navigation system based on the geophysical information is gradually realized by people. The integrated Gravity/Inertial navigation system is to use gravitational field measured by the sensors in the vehicle localize the vehicle on an existing gravity map, then utilize the result to correct the accumulated position errors of INS. The basic idea of Gravity aided navigation system is introduced, and the iterated closest contour point (ICCP) is used to perform the registration. The whole process is simulated in the experimental area by a visual manner.
AbstractList It is well known that the position errors of INS are accumulated with the time. In order to achieve high accuracy navigation, the vehicle must have other aided navigation methods. The process of receive signals such as GPS destroys the task of the under vehicle. The passive navigation system based on the geophysical information is gradually realized by people. The integrated Gravity/Inertial navigation system is to use gravitational field measured by the sensors in the vehicle localize the vehicle on an existing gravity map, then utilize the result to correct the accumulated position errors of INS. The basic idea of Gravity aided navigation system is introduced, and the iterated closest contour point (ICCP) is used to perform the registration. The whole process is simulated in the experimental area by a visual manner.
Author Buo, Xiu Chun
Yi, Cheng
Jing, Luo
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  organization: Sch. of Electr. Eng. & Autom., Tianjin Polytech. Univ., Tianjin, China
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Snippet It is well known that the position errors of INS are accumulated with the time. In order to achieve high accuracy navigation, the vehicle must have other aided...
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StartPage 62
SubjectTerms Extraterrestrial measurements
Geophysical measurements
Global Positioning System
Gravity
gravity aided navitation
iccp algorighm
Intelligent networks
Magnetic field measurement
Position measurement
Radio navigation
Sea measurements
simulation
Vehicles
Title The Simulation of ICCP Algorithm in the Gravity Aided Navigation
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