Integrated design method of gyro stabilized platform and attitude datum

The invention provides an integrated design method of a gyro stabilized platform and an attitude datum. According to the application requirement of independent design of imaging load in an aerial remote sensing system, with the integrated design of the gyro stabilized platform and the attitude datum, high-precision measurement of imaging load motion parameters can be accomplished and imaging loadis independently designed. The method comprises the steps: firstly, according to the motion relationship between frames of the gyro stabilized platform and the imaging load, an installation mode of inertial sensors on the three frames of the gyro stabilized platform is designed; then, inertial information measured by the inertial navigation of a flight carrier and the inertial sensors arranged onthe frames of the gyro stabilized platform is collected; then, the inertial measurement information is decomposed and transmitted to the imaging load by relative angle between the frames outputted bythe angle sensors at the se