At present, the control accuracy of wind tunnel flow field is difficult to meet the large aircraft requirement. In this paper, a multivariable model prediction control is introduced to design the flow field controller. To improve the ability to resist attack angle disturbance in a wind tunnel test, dynamic compensation of the attack angle is proposed to improve the predictive value of static pressure. Considering more new test conditions, a multi-model fusion method is used to solve the problem of establish...
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