2012 13th International Radar Symposium 2012
DOI: 10.1109/irs.2012.6233320
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SAR-based augmented integrity navigation architecture

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Cited by 15 publications
(7 citation statements)
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“…Figure 2 shows the overview of the incremental SfM workflow, which contains the following steps: (1) feature extraction; (2) feature matching; (3) geometric verification; (4) reconstruction initialization; (5) image registration; (6) triangulation; and (7) bundle adjustment. To generalize, the SfM approach might be divided into two main parts: the correspondence search phase (1-3) and iterative reconstruction phase (4)(5)(6). Based on these two phases, the estimation of the camera position for each image as well as a 3D reconstructed tie point, called a spare point cloud [20], can be done.…”
Section: The Principles Of the Structure From Motionmentioning
confidence: 99%
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“…Figure 2 shows the overview of the incremental SfM workflow, which contains the following steps: (1) feature extraction; (2) feature matching; (3) geometric verification; (4) reconstruction initialization; (5) image registration; (6) triangulation; and (7) bundle adjustment. To generalize, the SfM approach might be divided into two main parts: the correspondence search phase (1-3) and iterative reconstruction phase (4)(5)(6). Based on these two phases, the estimation of the camera position for each image as well as a 3D reconstructed tie point, called a spare point cloud [20], can be done.…”
Section: The Principles Of the Structure From Motionmentioning
confidence: 99%
“…A recently developed technique is the use of Synthetic Aperture Radar (SAR) and Interferometric SAR (InSAR) radar for navigation correction [4][5][6][7]. Radio waves used in this technique can be easily used during cloud cover, night, and rain, which makes this method universal and independent of the weather conditions.…”
Section: Introductionmentioning
confidence: 99%
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“…This problem can affect in particular medium-altitude long-endurance (MALE) UAV, which has to fly for thousands of kilometers before reaching its target. Cumulative drift (up to hundreds of meters) during a long endurance flight can lead the UAV to miss the planned target with catastrophic consequences on the mission [ 4 ]. Thus, future guidance systems for UAV autonomous missions have challenging requirements for high reliability and integrity.…”
Section: Introductionmentioning
confidence: 99%