The application provides a wind tunnel test model attitude angle calculation method,
electronic equipment and a storage medium, and belongs to the technical field of attitude angle calculation. The method comprises the following steps: S1, calibrating a double-shaft angle sensor by using a double-shaft
indexing head; S2, installing the double-shaft angle sensor in a model, and measuring the
pitch installation angle, the
yaw installation angle and the roll installation angle of the angle sensor relative to a model reference shaft
system; S3, changing the attitude angle of the model according to the wind tunnel test requirement, and measuring the
pitch angle and the roll angle of the angle sensor relative to a ground shaft
system by using the double-shaft angle sensor; S4, iteratively calculating the
yaw installation angle of the angle sensor relative to the ground shaft
system and the
pitch angle, the roll angle and the
yaw angle of the model reference shaft system relative to the ground shaft system, so as to obtain the
pitch angle, the roll angle and the yaw angle of the model reference shaft system relative to the ground shaft system; and S5, calculating the model attitude angle under a wind shaft system. The technical problem that only the
pitch angle and the roll angle can be measured, and the yaw angle cannot be measured in the prior art is solved.