The invention relates to the technical field of test measurement, and discloses an aircraft airspeed tube mounting attitude detection method, which comprises the following steps of: 1, establishing a conversion model of a measurement equipment coordinate system and an airframe coordinate system, and unifying the space reference of the measurement equipment coordinate system and the airframe coordinate system; 2, measuring the circumferential surface of the airspeed tube mounted on the airframe through measuring equipment, and converting the obtained parameters of the airspeed tube in a coordinate system of the measuring equipment into parameters in a coordinate system of the airframe; and 3, calculating the installation attitude of the airspeed tube based on the measured parameters of the airspeed tube in the airspeed body coordinate system.
本发明涉及试验测量技术领域,公开了一种飞机空速管安装姿态检测方法,包括以下步骤:步骤一:建立测量设备坐标系与机体坐标系的转换模型,将测量设备坐标系与机体坐标系空间基准统一;步骤二:通过测量设备对安装在机体上的空速管圆周面进行测量,并将得到的空速管在测量设备坐标系下的参数转换为机体坐标系下的参数;步骤三:基于测量得到的空速管在机体坐标系下的参数计算空速管的安装姿态。
Aircraft airspeed tube installation attitude detection method
一种飞机空速管安装姿态检测方法
2024-04-05
Patent
Electronic Resource
Chinese
IPC: | G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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