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- W2382201216 abstract "Based on the principle of moving-base gravimetry system,we deduce the mathematical models of measurement and error equations for airbrone gravimetry and gravity gradiometry.According to the inherent characteristic of the Earth gravity field and the basic theories of power spectral density,we analyze the specific requirements of the inertial stabilized platform in airbrone gravimetry and gravity gradiometry with known sensor error models for GPS receiver,stabilized platform,accelerometer,and gradiometer.By using the experiential models of acceleration and angular rate fitting from the practical flights of a Twin-Otter aircraft,we present the requirements for the stabilized platform by the numerical computation,that is,for the airbrone gravimetry with a resolution of 1 mGal,the requirements for the orientation error,stability and random noise of angular rate of the stabilized platform are 0.0005°,0.006°/h/ and 0.0003°/h,respectively,and for the airbrone gravity gradiometry with a goal of 1 E,the corresponding requirements for the stabilized platform are lowered to 0.5°,0.01°/h/(Hz)～(1/2),and 0.01°/h,respectively." @default.
- W2382201216 created "2016-06-24" @default.
- W2382201216 creator A5034003470 @default.
- W2382201216 date "2012-01-01" @default.
- W2382201216 modified "2023-09-26" @default.
- W2382201216 title "Requirement analysis of moving-base platform in airbrone gravimetry and gravity gradiometry" @default.
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