2022 3rd China International SAR Symposium (CISS) 2022
DOI: 10.1109/ciss57580.2022.9971441
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Analysis of Influencing Factors of Distributed Satellite InSAR Height-Measurement Accuracy based on Positioning Equation

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“…For instance, the value of the slant range directly influences height accuracy, with a 30 m slant range error typically resulting in a height error of 15 to 30 m. Additionally, azimuth time errors can lead to discrepancies between the estimated and actual satellite positions. If the satellite's velocity is 7.6 km/s, a 2 ms azimuth time error can result in a 15.2 m position estimation error, thus affecting the baseline vector derived from the subtraction of master and slave satellite vectors [46]. In cases with a 70 m ambiguous height, a 1 cm baseline error in the L-band biSAR system can introduce approximately 3 m of height error [33].…”
Section: Discussionmentioning
confidence: 99%
“…For instance, the value of the slant range directly influences height accuracy, with a 30 m slant range error typically resulting in a height error of 15 to 30 m. Additionally, azimuth time errors can lead to discrepancies between the estimated and actual satellite positions. If the satellite's velocity is 7.6 km/s, a 2 ms azimuth time error can result in a 15.2 m position estimation error, thus affecting the baseline vector derived from the subtraction of master and slave satellite vectors [46]. In cases with a 70 m ambiguous height, a 1 cm baseline error in the L-band biSAR system can introduce approximately 3 m of height error [33].…”
Section: Discussionmentioning
confidence: 99%
“…The accuracy of DEMs produced through InSAR is significantly influenced by various interferometric parameters, each affecting the height accuracy to different extents [15][16][17]. These parameters include flight altitude error, slant range error, interferometric phase error, and baseline error, with their impact on InSAR-derived heights ranging from least to most substantial [18]. Precision orbit determination is effectively employed to minimize flight altitude errors [19], and geometric calibration methods proficiently address slant range inaccuracies [20].…”
Section: Introductionmentioning
confidence: 99%