Method for Detecting Platform Pose Changes
An attitude change and detection platform technology, which is applied in the field of precision detection and can solve the problems such as the inability to accurately give the rotation component around a specific axis and the limited layout.
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specific Embodiment 1
[0015] See attached figure 1 And attached figure 2 , the present invention detects the method for platform attitude change, comprises the following steps:
[0016] Step 1: Arrange three detection points in the form of an equilateral triangle on the tested platform, the center of the equilateral triangle coincides with the center of the tested platform 1, and establish a spatial rectangular coordinate system X0YZ with the center of the tested platform 1 as the origin , the X-axis is perpendicular to one side of the equilateral triangle, let the normal vector of the platform be (0,0,1);
[0017] Step 2: Using a displacement detection instrument to monitor the displacement of the attitude change of the measured platform 1;
[0018] Step 3: Detect the displacement of the three detection points in step 1 after the posture change of the tested platform 1, and establish a space Cartesian coordinate system X`0Y`Z` with the center of the tested platform 1 as the origin, and use vect...
specific Embodiment 2
[0021] Step 1: Arrange three detection points A, B and C in the form of an equilateral triangle on the detected platform 1, △ ABC is an equilateral triangle, △ ABC The center of the center coincides with the center of the tested platform 1, and a space Cartesian coordinate system X0YZ is established with the center of the tested platform 1 as the origin. The normal vector is
[0022] Step 2: Using a displacement detection instrument to monitor the displacement of the attitude change of the measured platform 1;
[0023] Step 3: After detecting the attitude change of the tested platform 1, the vertical displacements D1, D2 and D3 of the three detection points in the step 1, and establish a space Cartesian coordinate system X`0Y`Z` with the center of the tested platform 1 as the origin, three The detection points A, B and C correspond to A`, B` and C` after the platform attitude changes, then
[0024]
[0025]
[0026] The platform normal vector n′ after the platform a...
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