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A platform and method for removing space debris from a child and a parent star

A space debris and sub-satellite technology, applied in the aerospace field, can solve problems such as the inability to remove low-orbit space debris at the same time, and achieve the effect of improving mission reliability, high reliability, and extending service life

Inactive Publication Date: 2018-11-13
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0008] The purpose of the present invention is to provide a space debris removal platform and removal method for the mother and child stars, so as to solve the problem that a large number of low-orbit space debris cannot be removed simultaneously in the prior art

Method used

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  • A platform and method for removing space debris from a child and a parent star
  • A platform and method for removing space debris from a child and a parent star

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Embodiment Construction

[0031] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0032] The invention discloses a platform for clearing space debris from the parent and child stars, such as figure 1 As shown, it includes a plurality of sub-stars 3 for removing space debris. Multiple sub-stars 3 have networking communication capabilities and have many advantages for removing space debris. Each sub-star 3 is equipped with a space debris removal device. Space debris removal The device includes a sub-star measuring device and a sub-star capturing device;

[0033] The parent star 1 is equipped with a parent star measuring device and a parent star capture device for assisting the child star 3 in removing space debris. The parent measuring device includes sensor components, and the sensor components include infrared sensors, visible light sensors, laser ranging sensors, and polarized light sensors. Etc., different attribute inf...

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Abstract

The invention discloses a child-mother satellite space debris clearing platform. The child-mother satellite space debris clearing platform includes a plurality of child satellites for clearing space debris; each child satellite is detachably connected the same mother satellite; the mother satellite is used for driving the child satellites to move among a multiple pieces of space debris; a space debris clearing device is arranged on each child satellite; and each space debris clearing device includes a child measurement device for measuring a pose of the space debris and a child satellite capturing device. A microsatellite is used as the mother satellite, and a plurality of micro-nano satellites are used as the child satellites; operations such as orbit transferring, closing and detailed survey, and capturing and de-orbiting can be completed coordinately; the child-mother satellite space debris clearing platform is low in cost, is fast in response speed, and is high in reliability; after the child satellites are released, the combined space debris observation network can acquire accurate debris pose information through coordinate observation; and the child satellites can independently complete de-orbiting operations, the mother satellite can directly go to next space debris to be cleared, time and energy can be saved, the benefits of space debris clearing can be increased, and the cost is reduced.

Description

【Technical field】 [0001] The invention belongs to the technical field of aerospace, and in particular relates to a space debris removal platform and a removal method of the parent and child satellites. 【Background technique】 [0002] In a broad sense, space debris can be divided into two types: Micrometeoroid and Space / Orbital Debris, and the operating area of ​​artificial space debris coincides with the operating area of ​​the orbiting service spacecraft, causing huge damage to human space exploration. Obstacles have attracted widespread attention. Because low-Earth orbit is the easiest to develop and has a wide range of uses, the number of available orbits continues to decrease, the satellite space density has reached a warning value, and unpredictable space collisions have begun to occur, so it is imperative to protect low-Earth orbit resources from space debris. [0003] According to the use of low-Earth orbit by humans in recent decades, from the first artificial earth...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/10B64G4/00
CPCB64G1/10B64G4/00
Inventor 刘勇杨家男冯乾李毅兰刘昆鹏王易周袁建平潘泉
Owner NORTHWESTERN POLYTECHNICAL UNIV
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