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Design and analysis of sub-index of high precision Airborne Gravity System |
Hong ZHANG1, Jin-Hong QU2,3, Zuo-Xi JIANG2,3, Meng WANG3, Xing-Su LI2,3 |
1. Beijing information technology School of Information Management, Beijing 100092, China 2. Key laboratory of Airborne Geophysics and Remote Sensing Geology, Ministry of Natural Resources, Beijing 100083, China 3. China Aero Geophysical Survey and Remote Sensing Center for Natural Resources, Beijing 100083, China |
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Abstract In order to meet the needs of development of high-precision airborne gravimeter , the sub-index design and analysis of high-precision airborne gravimeter were carried out, which provided the basis for the design of high-precision airborne gravimeter system. Based on the mathematical model of airborne gravimetry, this paper summarizes the main errors affecting airborne gravimetry, uses the theoretical model formula, deduces the error models of various influencing factors, and carries out the analysis and study of various errors, and sets reasonable sub-index by combining the relevant theoretical formula of airborne gravimetry. Accuracy can effectively control the sub item errors and ensure the accuracy of airborne gravity measurement is better than 0.6×10 -5 m/s 2.
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Received: 11 September 2018
Published: 10 April 2019
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速度/(km/h) 纬度误差/(‘) | 100 | 200 | 300 | 400 | 500 | 600 | 0.05 | 0.0059 | 0.0118 | 0.0177 | 0.0236 | 0.0295 | 0.0354 | 0.1 | 0.0118 | 0.0236 | 0.0354 | 0.0471 | 0.0589 | 0.0707 | 0.2 | 0.0236 | 0.0471 | 0.0707 | 0.0943 | 0.1178 | 0.1414 |
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The influence of latitude error on the Eotvos correction
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速度误差/(m/s) 飞行速度/(m/s) | 0.005 | 0.01 | 0.015 | 0.02 | 0.025 | 0.03 | 50 | 0.0808 | 0.1615 | 0.2423 | 0.3230 | 0.4038 | 0.4846 | 60 | 0.0823 | 0.1647 | 0.2470 | 0.3293 | 0.4116 | 0.4940 | 70 | 0.0839 | 0.1678 | 0.2517 | 0.3356 | 0.4195 | 0.5034 | 80 | 0.0855 | 0.1709 | 0.2564 | 0.3419 | 0.4273 | 0.5128 | 90 | 0.0870 | 0.1741 | 0.2611 | 0.3481 | 0.4352 | 0.5222 |
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The influence of velocity error on the Eotvos correction
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飞行速度/(m/s) 航向误差/(‘) | 200 | 220 | 300 | 400 | 500 | 600 | 0.1 | 0.0236 | 0.0259 | 0.0354 | 0.0471 | 0.0589 | 0.0707 | 0.5 | 0.1178 | 0.1296 | 0.1768 | 0.2357 | 0.2946 | 0.3535 | 1 | 0.2357 | 0.2593 | 0.3535 | — | — | — |
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The influence of course deviation on the Eotvos correction
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The gravity value perceived by the gravity sensor when the platform is not horizontal
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θ dθ | -30″ | -1’ | -2’ | -5’ | 1″ | -0.0235 | -0.0229 | -0.0215 | -0.0173 | 5″ | -0.1177 | -0.1143 | -0.1074 | -0.0867 | 10″ | -0.2355 | -0.2286 | -0.2148 | -0.1733 | 15″ | -0.3532 | -0.3429 | -0.3221 | -0.2600 | 20″ | -0.4710 | -0.4572 | -0.4295 | -0.3466 |
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The influence of platform measurement Error on horizontal acceleration correction
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名称 | 重力传感器 观测精度(静态) | 载体高程 测量精度 | 载体位置 测量精度 | 载体速度 测量精度 | 稳定平台角(或姿 态角)测量精度 | 同步精度 | 指标 | 优于0.3(10-5 m/s2) | 优于3 mm | 优于1 m | 优于0.02 m/s | 优于10″ | 优于1 ms |
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Precision requirements of sub-index of airborne gravity system
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