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Modeling Method of Space Manipulator Based on Differential Geometry

A technology of space manipulators and modeling methods, applied in special data processing applications, instruments, electrical digital data processing, etc., can solve problems such as lack of research results and methods

Active Publication Date: 2016-03-23
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the research process of the space manipulator, there is a requirement that the model of the space manipulator established can not only ensure the calculation efficiency and accuracy of the model, but also have a clear physical meaning. At present, there are no similar research results and methods in the literature search

Method used

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  • Modeling Method of Space Manipulator Based on Differential Geometry
  • Modeling Method of Space Manipulator Based on Differential Geometry
  • Modeling Method of Space Manipulator Based on Differential Geometry

Examples

Experimental program
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Effect test

Embodiment 1

[0067] Example 1, combining figure 1 , the steps of the differential geometry-based modeling method of the present invention are as follows:

[0068] Step 1: Select the zero position of the robotic arm system, and write the zero position joint vector S∈se(3), the mass center joint vector r, and the inertia matrix I.

[0069] Step 2: Calculate the positive definite symmetric matrix J related to the inertial parameters, and the coordinate position matrix M∈SE(3).

[0070] Step 3: Calculate the generalized velocity of each connecting rod by forward recursion.

[0071] Step 4: Given the generalized force F acting on the end effector n+1 , the generalized force of each connecting rod is calculated by reverse recursion.

[0072] Step 5: Write each quantity as a matrix expression to obtain the dynamic equation in compact form.

Embodiment 2

[0073] Example 2, combined figure 1 , figure 2 , the zero position of the robotic arm system studied by the present invention is selected in this way, the center of mass of the base and each link joint are selected as the origin of the base and the fixed connection coordinate system of the connecting rod at all levels, and the base coordinate system is recorded as 0 number, the connecting rods at all levels are marked as i (i=1,...,n), the fixed coordinate system of the end effector is marked as number (n+1), and the origin is selected at the end of the connecting rod. According to the robotics convention, the variables of each link joint are defined as

[0074]

[0075] with q i =0 is zero bit.

[0076] For the plane 2R free-flying space manipulator system, the zero joint vector S i =[001000] T ; centroid position vector r 0 =[000] T , r 1 =[a 1 00] T , r 2 =[a 2 00] T , where a 1 , a 2 respectively are the geometric parameters shown in the figure; the iner...

Embodiment 3

[0077] Example 3, combined figure 1 , figure 2 , the matrix J and the coordinate position matrix M∈SE(3) defined by the present invention are calculated as follows,

[0078] J i = I i - m i r ~ i 2 m i r ~ i - m i r ~ ...

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Abstract

The invention discloses a space manipulator modeling method based on different geometry. On the foundation that each level rigid body zero position of a space manipulator system is selected, initializing conditions such as a zero position joint vector, a centroid joint vector and an initial vector are calculated and given, and a matrix related to initial parameters and a coordinate position matrix are calculated. The generalized velocity of each connecting rod is calculated through forward recursion, and the generalized force of each connecting rod is calculated through reverse recursion. Each quantity is substituted into the matrixes, and a kinetic equation compact in form is written down. The model has the advantages of being uniform in modeling form and small in operating amount, improving calculation efficiency and accuracy of the space manipulator modeling, and improving the designing accuracy of the space manipulator. The space manipulator modeling method based on differential geometry can be applied to modeling of other space multi-rigid-body systems.

Description

technical field [0001] The invention belongs to the field of space manipulator model construction, in particular to a differential geometry-based modeling method of a space manipulator. Background technique [0002] As a spacecraft on-orbit maintenance equipment, the space manipulator can complete many tasks such as spacecraft maintenance, fuel replenishment, material transportation, and space garbage cleaning, and plays an important role in space activities. [0003] In the process of design and demonstration of space manipulator, accurate and simple mathematical model is the basis of research. However, the space manipulator works in a weightless environment in space, and there is a high degree of coupling between the floating base and the manipulator link. At the same time, due to the consideration of the economic cost caused by launching objects into space, the volume, mass and energy consumption of the space manipulator are greatly limited. Therefore, the traditional g...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F17/50
Inventor 夏红伟王常虹邓雅马广程宋效正翟彦斌
Owner HARBIN INST OF TECH
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