2022
DOI: 10.3390/rs14133089
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An Improved Independent Parameter Decomposition Method for Gaofen-3 Surveying and Mapping Calibration

Abstract: The Gaofen-3 (GF-3) satellite can provide digital elevation model (DEM) data from its interferogram outputs. However, the accuracy of these data cannot be ensured without applying a surveying and mapping (SAM) calibration process, thus necessitating geometric and interferometric calibration technologies. In this paper, we propose an independent parameter decomposition (IPD) method to conduct SAM calibration on GF-3 data and generate high-accuracy DEMs. We resolved the geometric parameters to improve the locati… Show more

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Cited by 4 publications
(4 citation statements)
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References 14 publications
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“…where µ =< r, v >, η =< r, n >, ς =< r, ŵ >, and < • > represents the inner product operation between vectors. Therefore, the representation of the unit look vector in the moving coordinate system can be calculated as [27][28][29]:…”
Section: Platform Three-dimensional Positioning Model Based On Insar ...mentioning
confidence: 99%
“…where µ =< r, v >, η =< r, n >, ς =< r, ŵ >, and < • > represents the inner product operation between vectors. Therefore, the representation of the unit look vector in the moving coordinate system can be calculated as [27][28][29]:…”
Section: Platform Three-dimensional Positioning Model Based On Insar ...mentioning
confidence: 99%
“…This approach achieved remarkable accuracies, with an interferometric phase precision of ±7.5 mm and baseline accuracy of 2 mm [23][24][25]. TanDEM-X's calibration success proved its efficacy and served as a blueprint for subsequent InSAR systems like Gaofen-3 and TH-2 satellites [26], promoting advancements in interferometric calibration. Additionally, numerous studies have focused explicitly on independent baseline calibration methods [27][28][29].…”
Section: Introductionmentioning
confidence: 97%
“…Synthetic aperture radar (SAR) satellites currently operating in orbit are all low Earth orbit (LEO) SAR satellites [1,2], the orbital altitudes of which are within 2000 km, with an average altitude of ~500-800 km. Owing to limited flight altitude, coverage area is small, the surveying and mapping belt is narrow, and the repeated observation period is long.…”
Section: Introductionmentioning
confidence: 99%