The invention discloses a real-time overbounding method for civil aviation satellite navigation integrity augmentation system errors. According to the method, a time sequence model is utilized to analyze the temporal correlation of pseudo-range errors, fat-tail error samples without the temporal correlation are obtained, and overbounding calculation is performed after normalization processing is performed on the fat-tail error samples through a generalized autoregressive conditional heteroscedasticity (GARCH) model, so that a stationarity model of temporal correlation errors is established; and a confidence upper limit of a standard deviation of the pseudo-range errors is determined, optimal pseudo-range error sequence length is determined, and therefore processing of the uncertainty and error non-stationarity of the model is realized. Through the method, an extra integrity risk cannot be introduced; and due to tighter overbounding, the protection level calculated in real time is lowerthan that calculated through a traditional method, and consequently the availability of a satellite navigation augmentation system is improved.