Submissive stabilization control method in process of capturing spatial irregular moving object

A technology of motion target and stable control, which is applied in the direction of program-controlled manipulators, manufacturing tools, manipulators, etc. It can solve the problems that the main body cannot effectively follow, damage the manipulator device, and the implementation method is simple.

Active Publication Date: 2020-10-13
SHANGHAI AEROSPACE CONTROL TECH INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The common way to capture a spacecraft in orbit is to lock the joints and then de-rotate for a target with known motion or stable motion. This method requires the joints of the manipulator to withstand the torsional moment when the target and the body move relative to each other. , but the implementation is simple, it only needs to judge the timing of catching the target, and then lock the joints. The disadvantage is that the robot arm cannot be used as a damper to derotate the target, and for irregular moving targets, the body cannot effectively follow the target movement, which may Generate excessive momentary torque and damage the mechanical arm device

Method used

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  • Submissive stabilization control method in process of capturing spatial irregular moving object
  • Submissive stabilization control method in process of capturing spatial irregular moving object
  • Submissive stabilization control method in process of capturing spatial irregular moving object

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Embodiment Construction

[0037] The present invention will be further elaborated below by describing a preferred specific embodiment in detail in conjunction with the accompanying drawings.

[0038] Such as figure 1 As shown, a compliant and calm control method in the process of capturing irregular moving targets in space includes the following steps:

[0039] S1, determining the optimization variables when the manipulator captures the target, the optimization variables include: damping time, terminal velocity, joint angular velocity and joint angular acceleration;

[0040] In order to make the damping fast, the optimization of time is one of the factors that need to be considered; secondly, preventing excessive joint angular velocity during the damping process is also a problem that needs to be considered in trajectory planning; finally, in order to match the actual engineering, the control The size of the torque is also the content that needs to be optimized. The modified genetic algorithm is used...

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Abstract

The invention discloses a submissive stabilization control method in the process of capturing a spatial irregular moving object. A track simultaneously balancing the joint angle moving magnitude of amechanical arm, the tail end distance moving magnitude, the joint angular speed magnitude, the damping time and the control moment magnitude is designed through a modified genetic algorithm, thus themechanical arm is quickly and safely stabilized, damping is generated for relative movement of the object and a body to perform despinning, and a new thought is provided for damping and stabilizing the mechanical arm after capturing.

Description

technical field [0001] The invention relates to the field of space robots, in particular to a compliant and stable control method in the process of catching irregular moving objects in space. Background technique [0002] Space operation is an important trend in the development of spacecraft in the future. During the mission of space operation, the end of the manipulator comes into contact with the captured target, and the resulting transient collision will disturb the spacecraft-manipulator system. The system flipped and became unstable. Due to the significant effect of the impact force in the process of capturing the target, it is necessary to study the control strategy in the process of capturing. [0003] The common way to capture a spacecraft in orbit is to lock the joints and then de-rotate for a target with known motion or stable motion. This method requires the joints of the manipulator to withstand the torsional moment when the target and the body move relative to ...

Claims

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Application Information

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IPC IPC(8): B25J9/16
CPCB25J9/1607B25J9/1633B25J9/1635B25J9/1664
Inventor 侯月阳卢山王奉文张竞天姜泽华尹俊雄
Owner SHANGHAI AEROSPACE CONTROL TECH INST
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