The invention relates to the technical field of
satellite control systems, provides a miniature
electromagnetic valve propulsion
system, and solves the problem that normal operation of a
propeller control system is affected by inaccurate
data processing due to influence of factors such as
noise and temperature in a
signal conversion process. According to the method, historical data of an
electromagnetic valve are processed in different periods, a control model with a specific period is constructed, prediction of a real-time flight control command and engine performance
simulation are achieved, and through comparison of real-
time data and prediction data, the performance of a
propeller is influenced, and driving power cannot be provided for a
satellite. And the
system can find and process abnormal data in time, so that the engine
control system can operate normally. According to the invention, the accuracy of
data processing is improved, the real-time monitoring and optimization of the performance of the
propeller are realized, and the stability of
satellite flight is improved.