Large-scale blocked space attitude combined measurement device and method and automatic object attitude adjustment method
A measuring device and space attitude technology, applied in the field of large-scale barrier space attitude combined measuring devices, can solve the problems of high technical cost, low measurement efficiency, large cumulative error, etc., and achieve strong system stability, convenient system use, and attitude measurement. high precision effect
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Embodiment 1
[0048] Such as figure 1 As shown, a large-scale barrier space attitude combination measurement device is proposed in this embodiment, including a measured object (1), a combined measurement device and three attitude adjustment mechanisms (3), and the measured object (6) determines There are fixed feature points A, B, and C that characterize its horizontal attitude, and it is connected with the attitude adjustment mechanism (3) and lifted to form a three-point support state to realize attitude adjustment; the combined measuring device includes three attitude probes (2) , three five-degree-of-freedom adjustment platforms (1), MEMS micro-inertial sensors (7), data converters (9), digital levels (8) and data processing terminals (10), three attitude probes (3) are respectively installed Clamped on the five-degree-of-freedom adjustment platform (1), and respectively in contact with three fixed feature points A, B, and C of the measured object (6); the MEMS micro-inertial sensor (7)...
Embodiment 2
[0055] This embodiment is realized on the basis of the posture combination measurement device provided in Embodiment 1, and a posture measurement method based on the device is proposed, including the following steps:
[0056] Step 1. The measured object is lifted by the attitude adjustment mechanism to achieve a three-point support state, and the MEMS micro-inertial sensor is installed on the measured object, and the five-degree-of-freedom adjustment platform is adjusted to adjust the vertical position of the attitude probe and the fixed characteristics of the measured object. point contact;
[0057] Step 2. The digital level is fixedly placed directly in front of the measured object, aiming at each attitude probe in turn to obtain the horizontal height from the feature points A, B, C to the reference plane, and combining the distance between each feature point to obtain the measured The initial attitude value of the object; at the same time, the angle between the X-axis and Y...
Embodiment 3
[0078] This embodiment is realized on the basis of Embodiment 2, and the coupling characteristics of sensor output change value and each attitude adjustment mechanism change amount are established, and the mathematical relationship model between the two is established as follows:
[0079] du 1 =f 1 (dc 1 ,dc 2 ,dc 3 ) (5)
[0080] du 2 =f 2 (dc 1 ,dc 2 ,dc 3 )
[0081] Among them, du 1 、 du 2 Respectively, the sensor X-axis, Y-axis output variation, dc 1 、dc 2 、dc 3 Respectively are the front, left and right jacking changes of the attitude adjustment mechanism.
[0082] Carrying out polynomial expansion on (5), and ignoring the components above the second order, we have:
[0083]
[0084] Transform (6) into matrix form, we can get:
[0085]
[0086] in, Correspondingly dv 1 = dc 1 , dv 2 = dc 2 , dv 3 = dc 3 , dv 4 = 2dc 1 dc 2 , dv 5 = 2dc 1 dc 3 , dv 6 = 2dc 2 dc 3 , dv 7 = dc 1 2 , dv 8 = dc 2 2 , dv 9 = dc 3 2 .
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