Identification method for space target rotation state based on binocular vision
A space target and rotation state technology, applied in the aerospace field, can solve problems such as the inability to guarantee the center point, the inability to identify the rotation axis and the rotation angular velocity, etc.
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[0083] (1) Approaching the observation operation target:
[0084] Control the body equipped with a binocular camera to approach the target so that it parks at point P near the target, such as figure 1 As shown, select two marker points A and B on the target, observe the movement of the two points through the binocular camera, take ΔT=1s, the given position vector is as follows (unit: cm):
[0085] r A0 =(300,400,155.27864) T ;r B0 =(500,200,244.72136) T
[0086] r A1 =(442.68513,310.12752,102.46599) T ;
[0087] r B1 =(423.83306,162.06127,358.82704) T ;
[0088] Compute the angular measure θ:
[0089]
[0090] Then satisfy |θ|>5° and |180-θ|>5°, so turn to step 2.
[0091] (2) Determine the direction vector of the rotation axis in the camera coordinate system:
[0092] Compute the vectors separately:
[0093] r flag =(r B0 -r A0 )×(r B1 -r A1 )=[-38028.76,-52958.39,-33383.66] T
[0094] r S = ...
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