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A dynamic control method and system for space non-cooperative target navigation capture

A technology of non-cooperative goals and control methods, applied in general control systems, control/regulation systems, adaptive control, etc. Meet the real-time requirements of the control algorithm and other issues, and achieve the effects of easy programming and software implementation, real-time calculation, and easy calculation code output

Active Publication Date: 2021-06-11
BEIJING INST OF SPACECRAFT SYST ENG
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, the working space of the free-floating system is limited due to the constant position of the center of mass of the system
Especially when capturing moving targets, the singularity of the workspace dynamics can cause system stability problems
At present, these methods have the following limitations in application: 1) Most of them assume that the base is in a free-floating state, that is, the base is not subject to any control; 2) Most of the dynamic models are iterative and recursive, which does not satisfy the derivation and realization of control algorithms; 3) The model has a large amount of calculation and does not meet the real-time requirements of the control algorithm

Method used

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  • A dynamic control method and system for space non-cooperative target navigation capture
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  • A dynamic control method and system for space non-cooperative target navigation capture

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specific Embodiment approach

[0093] The implementation process of the whole invention is as follows: figure 1 shown. The specific implementation is described in detail as follows:

[0094] (1) Establish the kinetic energy expression of each body. The calculation equation provided by the present invention is an open mathematical description, which is convenient to realize the calculation code output, and is based on a semi-model, semi-hardware control system and semi-physical simulation.

[0095] The kinetic energy expression of the base is set as

[0096]

[0097] Among them, v 0 and ω 0 is the velocity and angular velocity of the base relative to the inertial system, m 0 is the mass of the base, P 0 is the static moment of the base, given by the mass properties of the base, I 0 is the moment of inertia matrix of the base, given by the quality characteristics of the base, and 1 is a 3*3 unit matrix.

[0098] Similarly, the kinetic energy expression of the k-th arm of the m-th robotic arm is set ...

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Abstract

A dynamic control method and system for navigating and capturing non-cooperative space targets, aiming at the navigation and capture problem of space robots grabbing spin or rolling non-cooperative targets in orbit, this paper presents a dynamics of non-cooperative space target navigation capture Control Method. First, an analytical description of the kinetic energy of the space robot system is established. Secondly, the kinematic equation of the space robot is established. Finally, an analytical kinematics and dynamics model of the space robot system is established by using the Lagrangian equations of the second kind and pseudo-coordinate equations. This method is derived based on the theoretical method of vector mechanics, using matrix and vector operations, and the equations are analytical expressions with clear physical meaning. This method is convenient for the coupled analysis of the kinematics and dynamics of the space robot system, and is convenient for the realization of the model-based dynamic control algorithm, and the calculation amount is small, which is convenient for the real-time calculation of the control algorithm.

Description

technical field [0001] The invention relates to a dynamic control method and system for navigation and capture of space non-cooperative targets, belonging to the technical field of dynamic control. Background technique [0002] In-orbit service of space robots will play an increasingly important role in future space activities, such as satellite maintenance, large-scale space structure construction, space debris removal and other tasks, in order to reduce the risk of astronauts leaving the cabin and improve work efficiency. On-orbit service is especially suitable for non-cooperative satellites. Since faulty satellites generally do not have special capture devices and are often in a spinning or rolling state, it poses severe challenges to capture operations. [0003] The main difference between a space robot and a ground robot arm is that the base of the space robot is not fixed on the ground, but works in a microgravity environment. The dynamics and kinematics of the manipu...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B13/04
CPCG05B13/042
Inventor 葛东明王大轶史纪鑫谢宁邹元杰邓润然朱卫红柳翠翠仲维昆
Owner BEIJING INST OF SPACECRAFT SYST ENG
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