Aircraft attack angle correction curve acquisition method

The invention relates to an aircraft attack angle correction curve acquisition method. The method comprises the steps that step one, the measuring range and the type of an attack angle sensor are selected; step two, the installing area of the attack angle sensor is determined; step three, the installing position of the attack angle sensor is determined; step four, flight testing is performed; and step five, a correction curve is acquired. The problems of attack angle false alarm caused by inaccurate measurement of the attack angle in the flight can be solved by the method. The method has wide application prospect and has application value in the design of the complex pneumatic profile parts of the special aircraft. 本发明涉及种飞机攻角修正曲线的获取方法，该方法包括：步骤、选取攻角传感器量程和类型；步骤二、确定攻角传感器安装区域；步骤三、确定攻角传感器安装位置；步骤四、飞行试验；步骤五、取得修正曲线。由该方法解决了飞行中攻角测量不准确及其因此而引发的攻角误告警问题。此方法具有广阔应用前景，在特种飞机复杂气动外形部件的设计中具有应用价值。