Method for measuring positioning points based on laser tracker in docking process of airplane parts

A technology of laser tracker and aircraft components, which is applied in the direction of aircraft component testing, aircraft parts, measuring instruments, etc., and can solve problems such as complex working conditions, dangers, and data measurement fluctuations on site

Inactive Publication Date: 2012-06-27
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

However, this method also has the following problems: 1) Since there are many positioning and measuring points on the part, workers need to repeatedly guide the light to measure, the work intensity is high, and the measurement efficiency is low; 2) Hand-held target ball measurement is easy to c...

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  • Method for measuring positioning points based on laser tracker in docking process of airplane parts
  • Method for measuring positioning points based on laser tracker in docking process of airplane parts
  • Method for measuring positioning points based on laser tracker in docking process of airplane parts

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Embodiment Construction

[0051] The method for measuring positioning points in the docking process of aircraft components based on a laser tracker comprises the following steps:

[0052] Step 1. Select the TB or ERS point as the public observation point at the location of the docking site of the aircraft parts. The public observation point can be measured by the laser tracker, and the number of the public observation points is greater than 7;

[0053] Step 2. Use the laser tracker to measure the coordinates of public observation points, and obtain the measurement coordinates of these points in the measurement coordinate system of the laser tracker

[0054] Step 3. Combining target coordinates of public observation points and measuring coordinates Determine the mapping relationship between the laser tracker measurement coordinate system and the aircraft component global coordinate system; specifically:

[0055] (1) The transformation model function of the mapping between the laser tracker measure...

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Abstract

The invention discloses a method for measuring positioning points based on a laser tracker in a docking process of airplane parts. The method provided by the invention comprises the following steps of 1, establishing a model of transformation between an airplane global coordinate system and a laser tracker measure coordinate system according to common observation points, 2, acquiring current calculating positions of positioning measure points of airplane parts according to a process joint sphere centre position, and 3, controlling and driving a laser tracker to search current accurate positions of the positioning measure points of the airplane parts from the current calculating positions according to a cross helical search method and to carry out automatic measure. The method provided by the invention has the advantages that 1, an advanced laser measure technology is adopted so that the airplane assembling measure precision is improved; and 2, a measure process does not need artificial light introduction and full automatic search measure of a docking assembling process is realized according to an algorithm so that working efficiency and measure precision are greatly improved and working strength of workers is reduced.

Description

technical field [0001] The invention belongs to the technical field of positioning point measurement, in particular to a method for measuring positioning points in the docking process of aircraft components based on a laser tracker. Background technique [0002] The docking assembly of traditional aircraft large parts (docking of the front, middle and rear sections of the fuselage, wing and fuselage docking, etc.), using optical collimators and plumb bobs as measurement methods for component attitude adjustment, and using manual positioners to realize aircraft component support and docking . The results obtained by the measurement method based on these analog quantities not only have large errors, but also the data cannot directly reflect the current overall attitude characteristics of the aircraft components, and cannot provide effective guidance for its docking process. Therefore, the docking process of aircraft components completely depends on manual experience and manua...

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Application Information

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IPC IPC(8): G01C15/00G01B11/00B64F5/00B64F5/10B64F5/60
Inventor 李泷杲黄翔邓正平赵乐乐
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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