Dynamic position and attitude synchronization measurement method fusing inertial measurement information

A dynamic position and inertial measurement technology, applied to measurement devices, navigation through velocity/acceleration measurement, mapping and navigation, etc., can solve problems such as inability to meet accuracy requirements, limitations, and low measurement frequency, and achieve measurement accuracy and real-time performance. The effect of improving the performance, reducing the dynamic error, and improving the data rate of the pose measurement

Pending Publication Date: 2022-04-29
TIANJIN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The inertial measurement system represented by gyroscopes and accelerometers can autonomously sense the angular velocity and acceleration of the target's movement around the clock. It has the characteristics of high measurement frequency and strong anti-interference ability. The drift error of independent measurement of position and orientation diverges rapidly with time. , cannot meet the accuracy requirement
Limited by the speed of the transmitting station, the measurement frequency of wMPS is low, but its single measurement errors are independent of each other and have long-term stability. An external auxiliary system is required to be sensitive to the motion information within the measurement interval to achieve error compensation.

Method used

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  • Dynamic position and attitude synchronization measurement method fusing inertial measurement information
  • Dynamic position and attitude synchronization measurement method fusing inertial measurement information
  • Dynamic position and attitude synchronization measurement method fusing inertial measurement information

Examples

Experimental program
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Embodiment 1

[0029] An embodiment of the present invention provides a dynamic position and attitude synchronization measurement method fused with inertial measurement information, see Figure 1-Figure 4 , the method includes the following steps:

[0030] 101: Rigidly connect the position and attitude measurement target formed by the IMU and the wMPS photoelectric receiver, and use a three-coordinate measuring machine to measure the coordinates of the center of the photoelectric receiver and fit the IMU's own coordinate system to realize the unification of the observation objects of the wMPS and the IMU;

[0031] 102: Place the rigidly connected pose measurement target on the target to be measured and move with the target, use the laser transmitting station to measure the scanning angle of each receiver, and construct the geometric constraint relationship of the light plane; take the wMPS pose observation at the initial position as The initial value of the IMU state is updated, and the IMU ...

Embodiment 2

[0043] The following combined with specific examples, Figure 1-4 1. The specific calculation formula further introduces the scheme in Embodiment 1, see the following description for details:

[0044] Step 201: Arrange N transmitting stations in the space according to the requirements of measurement accuracy and range, and determine the rotation and translation relationship between the N transmitting stations and the global coordinate system by using the existing control field calibration method or standard scale calibration method;

[0045] Wherein, the step 201 is well known to those skilled in the art, and will not be described in detail in this embodiment of the present invention.

[0046] Step 202: Use 6 wMPS photoelectric receivers to form a pose measurement target, and rigidly connect the IMU to the pose measurement target (such as figure 1 As shown), use a three-coordinate measuring machine to measure the spherical center coordinates of the six photoelectric receivers...

Embodiment 3

[0103] Below in conjunction with specific data, the scheme in embodiment 1 and 2 is carried out feasibility verification, see the following description for details:

[0104] The high-precision linear guide is used to verify the dynamic measurement accuracy of wMPS assisted by IMU. The straightness error of the linear guide is measured by laser interferometer, and the maximum error is less than 0.05mm. The wMPS position and attitude measurement target is fixed on the linear guide rail translation platform for linear motion, and the wMPS and IMU data are combined to solve the spatial position of the position and attitude measurement target. The IMU measurement frequency is set to 80Hz. Using multiple measurement points on the motion trajectory to fit the spatial straight line, calculate the straightness error at each measurement point, and use the straightness RMSE (root mean square error) as a characterization index of the dynamic measurement error in the whole motion process. ...

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Abstract

The invention discloses a dynamic position and attitude synchronization measurement method fused with inertial measurement information, which comprises the following steps: rigidly connecting an IMU (Inertial Measurement Unit) with a pose measurement target formed by a wMPS photoelectric receiver, respectively measuring the spherical center coordinates of the photoelectric receiver by using a three-coordinate measuring machine, fitting the coordinate system of the IMU, and unifying the observation objects of the wMPS and the IMU; placing the rigidly connected pose measurement target on a measured target and moving along with the target, measuring the scanning angle of each receiver by using the laser emission station, and constructing a light plane geometric constraint relationship; the wMPS pose observation at the initial position is used as an IMU state updating initial value, and the IMU state is updated successively by using the angular velocity and the acceleration output by the IMU; and if a new wMPS measurement result exists in two adjacent IMU state updating processes, performing wMPS and IMU pose measurement data fusion to obtain a fused system state quantity, and outputting a final pose in combination with IMU self updating.

Description

technical field [0001] The invention relates to the field of large-space dynamic measurement, in particular to a measurement method for synchronous dynamic position and attitude fused with inertial measurement information. Background technique [0002] With the development of high-end equipment manufacturing technology in the aviation and aerospace fields represented by spacecraft and aircraft, intelligent manufacturing has become an important trend and research hotspot, and it is an important measure to promote equipment manufacturing to high-end and build a manufacturing power. As a key way to obtain geometric quantity information, measurement is gradually integrated into all aspects of equipment manufacturing, which is a necessary prerequisite for the realization of intelligent manufacturing. Traditional single-objective and static measurement modes are difficult to meet many requirements such as efficiency and real-time performance. It is urgent to study high-precision, ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C21/16
CPCG01C21/165G01C21/183
Inventor 史慎东邾继贵杨凌辉林嘉睿任永杰
Owner TIANJIN UNIV
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