A SHA-Based Method for Lifetime Prediction of Spacecraft ACS Missions
A life prediction and spacecraft technology, applied in the direction of instruments, simulators, control/regulation systems, etc., can solve problems such as mission life termination, system performance degradation, and inability to reflect dynamic interaction between components and systems, so as to overcome difficulties in obtaining and avoiding The effect of incomplete information
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[0023] The technical solution of the invention will be described in detail below in conjunction with the accompanying drawings.
[0024] figure 1 The shown mission life prediction method for spacecraft attitude control system based on stochastic hybrid automata is implemented by a system including: SHA module, on-orbit environment temperature prediction module, similarity module, calculation & statistical analysis module. The similarity module processes the information of the historical spacecraft through the similarity algorithm to obtain the component on-orbit reliability model of the current spacecraft; establishes the component SHA according to the component performance degradation model and the component reliability model obtained in the previous module, and then combines DFT to obtain the The subsystem SHA consists of the SHA module, which is used to simulate the random mixed movement of the spacecraft subsystems in orbit; according to the historical time series of the t...
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