The invention discloses a
geosynchronous orbit determination and parameter determination method based on differential algebra. A
kinetic model described based on
geosynchronous satellite orbit elements is selected and used, use of a relatively greater integration step in a numerical integration process is avoided and appearance of singular points is avoided for the
kinetic model, moreover, a perturbative force item is added in the
kinetic model, polynomial form integration is executed, thus, obit statuses and
spacecraft parameters are obtained, high-order prediction is executed for the obtained parameters, and meanwhile, high-order prediction of observed quantity is executed; by means of nonlinear information of the kinetic model and an observation model,
estimation accuracy is improved; in combination with actual observed values of a
spacecraft, high-order prediction values of the obit status and the
spacecraft parameters are updated and high-order estimated values as initial values are obtained; and by repeating the implementation process above,
geosynchronous orbit determination and parameter determination can be completed. The method provided by the invention not only can improve accuracy of obit
estimation and realize high-precision
estimation of the parameters, but also can greatly reduce calculation cost.