2016
DOI: 10.1007/s10291-016-0590-5
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Shipborne high-accuracy heading determination method using INS- and GPS-based heading determination system

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Cited by 11 publications
(5 citation statements)
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“…There are also related works on collision avoidance such as those of Flåten and Brekke [18] and Chen et al [19]. Works similar to ours that used sensor fusion in deriving a more accurate heading for navigation were by Hu and Huang [20] and Juang and Lin [21] while there were others that focused on the improved position and attitude aside from the heading such as those by Jaroś et al [22], Bryne [23], Núñez et al [24], and Feng-de et al [25].…”
Section: Introductionmentioning
confidence: 77%
“…There are also related works on collision avoidance such as those of Flåten and Brekke [18] and Chen et al [19]. Works similar to ours that used sensor fusion in deriving a more accurate heading for navigation were by Hu and Huang [20] and Juang and Lin [21] while there were others that focused on the improved position and attitude aside from the heading such as those by Jaroś et al [22], Bryne [23], Núñez et al [24], and Feng-de et al [25].…”
Section: Introductionmentioning
confidence: 77%
“…The new technology not only provides high-precision positioning and depth information [7][8][9], but also expands the technical means of obtaining information on oceanographic surveys. For example, in order to improve the accuracy of ocean measurement and reduce the input of artificial stations, researchers around the world are committed to the use of high-precision GNSS [10] for shipborne navigation [11,12] measurement in recent years.…”
Section: Introductionmentioning
confidence: 99%
“…An inertial baseline vectors by GNSS relative positioning, and then attitude information can be obtained (Medina et al 2020. Compared with an inertial navigation system, the multi-antenna GNSS attitude determination method has the advantages of low cost and no accumulated errors over time (Daneshmand andLachapelle 2017, Hu andHuang 2017). A multi-antenna GNSS can not only obtain high-precision attitude independently, but also provide attitude reference information for a low-cost inertial navigation system.…”
Section: Introductionmentioning
confidence: 99%