Title of article
INS/VisNav/GPS relative navigation system for UAV
Author/Authors
Wang، نويسنده , , Xiaogang and Cui، نويسنده , , Naigang and Guo، نويسنده , , Jifeng، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2013
Pages
7
From page
242
To page
248
Abstract
A methodology for fusing dates from Inertial Navigation System (INS), Carrier-Phase Differential Global Positioning System (CDGPS), and Vision-Based Navigation System (VisNav) is presented. The hierarchically distributed architecture based on information filtering is developed to estimate the relative attitude, position and velocity between the leader and follower in formation. Simulation results show that INS/VisNav/GPS relative navigation system has higher accuracy compared to INS/GPS and INS/VisNav systems.
Keywords
Vision-based sensor , information filtering , formation flight , Relative navigation
Journal title
Aerospace Science and Technology
Serial Year
2013
Journal title
Aerospace Science and Technology
Record number
2230979
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