The present invention relates to a method,
system, and terminal for measuring operating parameters of a shadow
rocket, and belongs to the technical field of shadow
rocket operations. The method comprises the following steps: identifying and collecting the
radial velocity, cloud position,
cloud height, and
wind speed of a target cloud layer; calculating the average
radial velocity of the target cloud layer based on the
radial velocity; determining the initial launch
azimuth of the shadow
rocket based on the average radial velocity and a reference direction; calculating the angle between the cloud movement
velocity vector and the reference direction based on changes in the cloud position; calculating the
wind field correction angle between the
resultant velocity vector of the
wind field and the cloud movement and the reference direction based on the
wind speed; constructing a dynamic state equation for the launch
azimuth of the shadow rocket based on the initial launch
azimuth, the angle between the cloud movement
velocity vector and the reference direction, the
wind field correction angle, and the
cloud height; and solving the equation based on the fourth-order Runge-Kutta method to obtain the final launch azimuth. The present invention has the beneficial effect of improving the accuracy and effectiveness of rain enhancement and hail prevention operations.