The invention provides a
satellite constellation simulation method based on a native set model. The
satellite constellation simulation method comprises the following steps that a current
view angle rotation matrix is obtained through calculation according to the current moment; and calculating a
satellite orbit. At the T0 moment of each circle, calculating satellite coordinate points contained at the starting and ending moments of the current circle to form a
satellite orbit, calculating the satellite coordinate positions by introducing a front-end
library, when the next circle arrives, calculating the
satellite orbit of the current circle again at the T0 moment of the circle, and updating and displaying the
satellite orbit; introducing a front-end
library to calculate a satellite coordinate position; the satellite
orbit and the
view angle keep the same
view angle rotation matrix for rotation transformation. According to the method, the
algorithm efficiency is greatly improved, the interaction process of the front end and the rear end is saved, the calculation and display efficiency of the satellite
orbit is improved and the rendering performance is improved on the premise that the display effect of satellite
simulation is not influenced, and the native model supports dynamic updating, so that the geometrical shape and the material can be modified during operation, and re-creation is not needed.