The function of SINS in airborne vector gravimetry is to measure the specific force,but standalone SINS can not satisfy the precision,so usually SINS/DGPS integrated navigation using Kalman Filtering is applied to improve the precision.

Then the precision of the determination of the acceleration vector under stable and kinetic conditions is analyzed respectively based on CHAGS observation,and the accuracy is second mGal,which is the same as the precision in theory and Absolutely satisfies the demand of the airborne vector gravimetry.

Research on space covariance function s characteristic during downward continuation of airborne gravity measurement data;

Thus,in the dynamic airborne gravity measurement (airplane as an aircraft) the key problem is to separate the gravitation from inertia effectively.

Filtering algorithm of airborne gravimetry based on SINS;

Filtering and processing for the airborne gravimetry data;

Fundamental Theory and Application of Airborne Gravity Gradiometry;

The principles of airborne gravimetry and airborne gravity gradiometry are introduced and discussed.

The basic concept and the analytical model of the airborne gravimetry system are introduced first, then the components of the system and their main functions are discussed in detailed.