On-orbit service and maintenance verification method and system

A verification method and cubic technology, which is applied to launch systems, instruments, aerospace vehicles, etc., can solve the problems of occupying space station resources and time consumption for many times, and achieve the effect of facilitating the handling of emergencies.

Active Publication Date: 2021-01-01
BEIJING INST OF SPACECRAFT SYST ENG
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

If it is carried out separately and decentralized, it will consume a lot of time and need to occupy...

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  • On-orbit service and maintenance verification method and system
  • On-orbit service and maintenance verification method and system
  • On-orbit service and maintenance verification method and system

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Embodiment Construction

[0045] In order to more clearly describe the embodiments of the present invention or the technical solutions in the prior art, the following will briefly introduce the drawings that are used in the embodiments. Apparently, the drawings in the following description are only some embodiments of the present invention, and those skilled in the art can also obtain other drawings according to these drawings without creative efforts.

[0046] When describing the embodiments of the present invention, the terms "vertical", "transverse", "upper", "lower", "front", "rear", "left", "right", "vertical", " The orientation or positional relationship expressed by "horizontal", "top", "bottom", "inner" and "outer" is based on the orientation or positional relationship shown in the relevant drawings, which are only for the convenience of describing the present invention and simplifying the description, and It is not to indicate or imply that the device or element referred to must have a particu...

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Abstract

The invention relates to a manned spacecraft on-orbit service and maintenance verification method. The method comprises the following steps of a building a test environment, transporting materials required by on-orbit verification to an extraterrestrial space station, and quickly building the test environment by utilizing the existing resources of a manned aerospace system and the flexible controlcapability of an astronaut; b assembling materials in a cubesat module form in a space station cabin, and carrying out on-orbit comprehensive detection on the materials; and c releasing the target inthe materials out of the space station cabin, and performing an approaching observation test and a net capturing test on the target. Verification is carried out on the manned spacecraft on-orbit service and maintenance technology, and compared with other technical verification methods, the method has the advantages of being good in technical basis, high in supporting capacity, small in task risk,large in number of guarantee resources, low in test cost, high in efficiency, comprehensive in verification and the like.

Description

technical field [0001] The invention relates to an on-orbit service and maintenance verification method and system. Background technique [0002] With the rapid development of aerospace technology, on-orbit service and maintenance has become an important development direction, which has attracted widespread attention from the international community. [0003] On-orbit service and maintenance technology is an important field for the development of space technology in the future. Its purpose is to ensure the stable and reliable operation of my country's space assets and improve the comprehensive use efficiency of my country's space assets. [0004] On-orbit maintenance is mainly a series of technical means adopted to enhance the use value of high-value cubesats and protect the space environment. Its main tasks include: inspection inspection, module replacement, auxiliary deployment, on-orbit refueling, control takeover, auxiliary Orbit change, debris active removal, on-orbit ...

Claims

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Application Information

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IPC IPC(8): B64G1/12B64G4/00B64G1/10B64G1/00B64G99/00G01M99/00
CPCB64G1/12B64G4/00B64G1/10B64G1/005G01M99/008B64G2004/005B64G99/00
Inventor 陈晓光齐玢李恩奇张志贤胡骏张柏楠
Owner BEIJING INST OF SPACECRAFT SYST ENG
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