基于一种头锥外形对超声速飞行嵌入式大气数据测量系统进行了原理、仿真及试验研究。结果显示,FADS测量结果较好的考虑了实时风场变化的飞行来流参数,马赫数测量偏差小于3%,攻角、侧滑角测量偏差小于1°。嵌入式大气数据测量技术在临近空间飞行器飞行控制、吸气式发动机控制和高精度气动辨识等专业领域具有广泛的应用前景。 Based on a kind of nose profile, the principle, simulation and experimental research of supersonic flight embedded atmospheric data measurement system are carried out. The results show that the FADS measurements take into account the variation of flight flow parameters in real-time wind field, the deviation of Mach number is less than 3%, and the deviation of attack angle and side slip angle is less than 1 °. Embedded atmospheric data measurement technology has broad application prospects in the fields of flight control, aspirated engine control and high-precision aerodynamic identification.