Fast space robot simulation modeling method and system

A technology of space robots and manipulators, applied in manipulators, program-controlled manipulators, manufacturing tools, etc., can solve problems such as large-scale software, complex control program interface processing, and poor autonomous controllability of codes, so as to avoid black boxes and reduce environmental compatibility sexual effect

Pending Publication Date: 2022-07-01
CHINA ACADEMY OF SPACE TECHNOLOGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Most of them are commercial software, and some are open-source software, but they all have the following disadvantages: large-scale software, complex algorithms, poor modularity, poor self-controllability of codes, and complicated interface processing with self-developed control programs, involving A lot of debugging work
[0004] At present, there are no public literature reports and patents at home and abroad that are identical to the simulation modeling method of the modularized fast space robot proposed in this patent.

Method used

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  • Fast space robot simulation modeling method and system
  • Fast space robot simulation modeling method and system
  • Fast space robot simulation modeling method and system

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Embodiment Construction

[0046] The present invention will be further elaborated below in conjunction with the examples.

[0047] The process of realizing the simulation modeling of the space robot in the present invention is as follows:

[0048] (1) Establish the kinematics model of the manipulator. The model input is the joint angle q of the manipulator j , joint angular velocity and joint angular acceleration (The subscript j represents the j-th arm), and the output is the position r of each arm of the manipulator relative to the coordinate system (m system) of the manipulator. mj ,speed with acceleration (see figure 1 ).

[0049] (1.1) Calculate the relative motion angular velocity Ω of each arm relative to the inscribed arm j and angular acceleration The calculation formulas are and where l j is the unit direction vector for each joint rotation;

[0050] (1.2) Calculate the angular velocity ω of each arm relative to the coordinate system (m system) of the robot arm installation ...

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Abstract

The invention relates to a quick space robot simulation modeling method. A joint angle, a joint angular velocity, a joint angular acceleration and a flywheel control moment of a mechanical arm are used as inputs; and the kinematics model of the mechanical arm, the mass center kinematics model of the space robot, the installation kinematics model of the mechanical arm, the reverse kinematics model of the mechanical arm and the forward attitude kinematics model of the base are solved circularly according to the preset time step length, and a kinematics simulation data sequence of the base and the mechanical arm of the space robot is solved. Modularized modeling is carried out on the space robot base and mechanical arm dynamics, researchers can independently develop simulation modules of the base and all mechanical arms carried by the base, and then module association calculation is carried out through a positive and negative dynamics mixing method and a space composite kinematics method. The above characteristics help researchers to quickly and efficiently realize space robot simulation modeling.

Description

technical field [0001] The invention belongs to the technical field of on-orbit service and maintenance of space vehicles, and relates to a simulation modeling method for a modular and fast space robot. Background technique [0002] On-orbit service and maintenance is one of the frontier hotspots in aerospace technology. After the service vehicle approaches the space target, it implements service operations such as close-range observation, refueling, auxiliary orbit change, module replacement, and component maintenance, which can achieve the target satellite's service operations. On-orbit fault recovery and life extension, so as to continue to exert on-orbit application value and generate great economic benefits. [0003] The use of space robot satellites with robotic arms is the most direct method to implement close-range service operations on target satellites, especially for delicate operation tasks such as module replacement and component repair. The dynamic simulation ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B25J9/16
CPCB25J9/1605
Inventor 黄良伟李志蒙波黄剑斌吴耀军黄龙飞庞羽佳张志民韩旭
Owner CHINA ACADEMY OF SPACE TECHNOLOGY
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