The invention discloses a
spacecraft system disturbance
estimation method with random suppression intensity of measured
noise, which belongs to the technical field of disturbance
estimation of
spacecraft systems, and comprises the following steps of: 1, establishing a
nonlinear model of a
spacecraft system considering the measured
noise, and accurately representing the dynamic behavior of a spacecraft in a complex environment by using the model; 2, a variable-order filter with independent parameters is established, the designed filter has the same
cascade structure as the observer, and therefore the parameters of the filter and the observer are mutually independent and not coupled; and step 3, aiming at an observer parameter adjustment problem, adopting an undetermined coefficient method, solving a proposed ESO
characteristic equation of filtering and a
characteristic equation of an expected configured pole, carrying out coefficient comparison on the two equations, and determining an observer parameter. According to the method, the parameters of the filter are increased along with the increase of the order of the filter, and the sum of the parameters of the observer is equal to the order of the observer, so that the problem of excessive parameterization is avoided, and arbitrary pole assignment is realized.