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Six-dimensional position and orientation precision test method of space mechanical arm based on air flotation system

A technology of a space manipulator and a testing method, which is applied in the direction of measuring devices, instruments, and optical devices, and can solve problems such as small joint drive torque, low arm stiffness, and ground testing problems

Inactive Publication Date: 2011-09-07
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Since the space manipulator is designed for the microgravity environment in space, its joint drive torque is small and the stiffness of the arm is low. However, due to the influence of gravity on the ground test, the six joints of the space manipulator cannot follow the plan. The path moves to the specified pose, which makes the ground test of the six-dimensional pose accuracy of the space manipulator a technical problem

Method used

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  • Six-dimensional position and orientation precision test method of space mechanical arm based on air flotation system
  • Six-dimensional position and orientation precision test method of space mechanical arm based on air flotation system
  • Six-dimensional position and orientation precision test method of space mechanical arm based on air flotation system

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specific Embodiment approach 1

[0050] Specific implementation mode one: as figure 1 As shown, the tested space manipulator in the test method described in this embodiment consists of the first joint 1, the second joint 2, the first arm 7, the third joint 3, the fourth joint 4, the second arm 8, The fifth joint 5 and the sixth joint 6 are sequentially connected to form; the test method is realized based on an air flotation system including an air flotation platform 11, an air foot 12, a supporting wheel 13, a manipulator support frame 14 and a balance weight 15;

[0051] The concrete process of described test method is:

[0052] Step A, expand the space manipulator and install it on the air flotation system to simulate the microgravity environment, and install the 6D sensor in the 6D laser tracker:

[0053] Step A1, release the constraint of the base flange part of the space manipulator, and place the space manipulator released from the constraint on the upper end surface of the air-floating platform 11 (th...

specific Embodiment approach 2

[0103] Specific embodiment two: In step D of this embodiment, the specific process of six-dimensional pose accuracy calculation is as follows:

[0104] Step D1, calculate the absolute position accuracy of the six-dimensional pose of the space manipulator:

[0105] The combined absolute position error of the combined measured value of the k-th measured configuration i and j is:

[0106] E k ij = ( x k ij - x k ) 2 + ( y k ij - y k ) 2 + ( ...

specific Embodiment approach 3

[0117] Specific implementation mode three: as figure 1 As shown, in step A3 of this embodiment, a ball joint 16 is provided between the lower end of the air foot 12 and the air bearing platform 11 .

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Abstract

The invention provides a six-dimensional position and orientation precision test method of a space mechanical arm based on an air flotation system, relating to a position and orientation precision test method of a space mechanical arm. In order to imitate a microgravity environment so as to test the position and orientation precision of the space mechanical arm at the ground, the method mainly comprises the following steps of: spreading the space mechanical arm and arranging the space mechanical arm on the air flotation system to imitate the microgravity environment; measuring and calculatingthe transformation matrix of a second target relative to a first target on an installation flange of the mechanical arm; measuring and calculating the transformation matrix of a third target relativeat the end of the mechanical arm relative to the second target; combining with the two position and orientation matrixes to obtain a coordinate transformation matrix of an end tool coordinate system E under a mechanical arm installing coordinate system M so as to test the position and the orientation of the end of the space mechanical arm; comparing the tested position and orientation with the theoretical position and orientation to obtain the position and orientation precision of the end of the space mechanical arm. The method imitates and reappears the space microgravity environment with the air flotation system, and guarantees the ground position and orientation precision tested by the developed space mechanical arm.

Description

technical field [0001] The invention relates to a method for testing the pose accuracy of a space manipulator, and relates to the technical field of space manipulator applications. Background technique [0002] With the advancement of technology, human activities are constantly expanding into space. According to statistics, an average of 80 to 130 satellites are launched each year in the world, but 2 to 3 satellites fail to enter orbit correctly, and among the satellites correctly entered orbit, 5 to 10 satellites are in the early stages of life (the first 30 days after orbit) ) that fails, which leads to huge economic losses. In order to recover the losses as much as possible, various countries are researching on-orbit service technology with space manipulators as the means of operation for the purpose of satellite maintenance and life extension. The current in-orbit services mainly include ORU (Orbital replacing unit) replacement, fuel supply, cleaning of abandoned satel...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01B11/00
Inventor 刘宇倪风雷刘宏徐文福
Owner HARBIN INST OF TECH
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