Non-axisymmetric carrier rocket load shedding control method and storage device

The invention provides a non-axisymmetric carrier rocket load shedding control method and a storage device. The method comprises the steps that standard trajectory design data, launching point geographic information data and launching window forecast high-altitude wind data are acquired; calculating launch data, high-altitude wind data, a transformation matrix from a launch system to an arrow system, a transformation matrix from a geocentric system to the launch system and a transformation matrix from a local horizontal system to the geocentric system at the time moment; calculating the projection of the unit wind vector at the moment in a transmitting system; calculating a rolling program angle theoretical value sequence corresponding to the time sequence; performing numerical fitting on the rolling program angle theoretical value sequence to obtain an engineered rolling program angle binding value sequence; calculating a first-order difference of the rolling program angular binding value sequence to obtain