Abstract:
Regularization method for differential equation of comets' motion is used. Numerical integration of the equation of motion of 10 short-period comets during the period of 1800 to 2204 with the use of osculating elements of the large planets is done. The high efficiency of this method for short-period comets study is demonstrated. efficiency of this method for short-period comets is shown.
Keywords:numerical integration, differential equation of motion, method of the osculation elements.