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

Pending Publication Date: 2021-11-26
SOUTHWEAT UNIV OF SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

One is to use multiple transfer stations of a single device to measure to avoid feature point occlusion, and to realize object attitude measurement through the unified coordinate system of the common reference point. Station will form a large cumulative error, so its application is limited
The second is to carry out multi-station collaborative measurement through multiple identical or different devices, and solve the object attitude through data fusion to improve the measurement accuracy and environmental adaptability of the system, such as the coordinated measurement of laser tracker and coordinate measuring arm or optical scanner, iGPS Measurement network construction, etc., but its technical cost is high, and measurement accuracy is greatly affected by the number of equipment and station layout methods

Method used

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  • Large-scale blocked space attitude combined measurement device and method and automatic object attitude adjustment method
  • Large-scale blocked space attitude combined measurement device and method and automatic object attitude adjustment method
  • Large-scale blocked space attitude combined measurement device and method and automatic object attitude adjustment method

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Experimental program
Comparison scheme
Effect test

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 .

[00...

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Abstract

The invention provides a large-scale blocked space attitude combined measuring device. The large-scale blocked space attitude combined measuring device comprises a measured object, a combined measuring device and an attitude adjusting mechanism; the measured object is determined to have fixed feature points A, B and C representing the horizontal attitude of the measured object, and is connected with the attitude adjusting mechanism for jacking to form a three-point supporting state so as to realize attitude adjustment; the three attitude probes are respectively clamped on a five-degree-of-freedom adjusting platform and are respectively in contact with three fixed feature points of a measured object; the MEMS micro inertial sensor is arranged on a measured object, and the output end of the MEMS micro inertial sensor is connected to the data processing terminal through the data converter; the digital level gauge is installed right in front of a measured object, observes the three attitude probes at the same time, and outputs the horizontal height of each feature point; and the data processing terminal is used for resolving the real-time attitude of the measured object according to the data output by the sensor and the horizontal height of the feature point. According to the scheme, instrument intervisibility conditions can be changed, the problem that measured points are blocked in large-scale attitude measurement is solved, accumulated errors are reduced, and the measurement precision is improved.

Description

technical field [0001] The invention relates to the technical field of precision measurement of object attitude, in particular to a large-scale barrier space attitude combined measurement device and method, and an object attitude automatic adjustment method. Background technique [0002] With the rapid development of aerospace, shipbuilding and other industrial fields, the precision measurement technology of large-scale space objects plays an important role in the assembly, docking and quality inspection of large and complex equipment, and has been increasingly valued by researchers. At present, there are many space attitude measurement equipment, including total station, laser tracker, iGPS, etc. However, in the large-scale range of several meters to hundreds of meters, due to the characteristics of large space span and complex on-site environment, there are still many problems in space attitude measurement. problem. Among them, due to factors such as the large size and co...

Claims

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Application Information

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IPC IPC(8): G01C21/16
CPCG01C21/165Y02T90/00
Inventor 马国鹭刘丽贤
Owner SOUTHWEAT UNIV OF SCI & TECH
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