At present， the big aviation countries already have mature gust wind tunnel test technology， but which is relatively back? ward in China， especially the gust wind tunnel tests equipment and technology of full aircraft model are lack. In this paper， a gust generator， a five-degree-of-freedom suspension system and a full elastic aircraft model are developed， and the wind tunnel tests of the whole model are carried out. The test results show that the gust field is stable， and the deviation of the gust velocity between the two ends and the center of the wind tunnel is less than 25%. The support stiffness of the model suspension system is small and the stability is good， which can meet the requirements of the gust wind tunnel test. The simulation results of the non-uniform gust field are close to those of the wind tunnel test， and the error of the moment of the wing root is less than 15%， and the error of wing tip overload is less than 0.2g.