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介绍一种为得到高速飞行器表面各部分的热应力、应变、结构膨胀量等高温力学性能参数而设计的瞬志气动力模拟加热控制系统。试验结果表明，本控制系统的控制结果与设定曲线符合良好。并可对非线性瞬志加热过程进行高精度的动态控制。
An instantaneous aerodynamic simulation heating control system designed to obtain the high temperature mechanical performance parameters such as thermal stress, strain and structure expansion of various parts of the surface of a high-speed aircraft is introduced. The test results show that the control results of this control system are in good agreement with the setting curve. And can be non-linear instantaneous heating process for high-precision dynamic control.