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A Rapid Deployment Architecture for Multi-Micro-Nano Satellites Oriented to On-orbit Service for Non-Cooperative Targets

A non-cooperative target, micro-nano-satellite technology, applied in the field of multi-micro-nano-satellite rapid deployment structure

Active Publication Date: 2022-04-08
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Aiming at the problem of rapid and accurate delivery and deployment of cluster members existing in the existing micro-nano satellite cluster on-orbit service technology, the present invention proposes a polyhedron frame structure for cluster micro-nano satellite storage storage and quick release deployment

Method used

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  • A Rapid Deployment Architecture for Multi-Micro-Nano Satellites Oriented to On-orbit Service for Non-Cooperative Targets
  • A Rapid Deployment Architecture for Multi-Micro-Nano Satellites Oriented to On-orbit Service for Non-Cooperative Targets
  • A Rapid Deployment Architecture for Multi-Micro-Nano Satellites Oriented to On-orbit Service for Non-Cooperative Targets

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Embodiment Construction

[0029] In order to make the object, technical solution and effect of the present invention clearer and clearer, the following examples are given to further describe the present invention in detail. It should be pointed out that the specific implementations described here are only used to explain the present invention, not to limit the present invention.

[0030] Such as figure 1 As shown, it is an overall schematic diagram of the multi-micro-nano-satellite rapid deployment structure for non-cooperative target on-orbit service of the present invention, which mainly includes 3 parts: a regular dodecahedron frame 1, a hook assembly 2 micro-nano-satellite body 3; The dodecahedron frame 1 adopts the dodecahedron structure as the skeleton, and the frame structure is a structure capable of quickly releasing micro-nano satellites and realizing adaptive adjustment of space attitude. Since the opposite sides of the dodecahedron are parallel to each other and the vertical line of the tw...

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Abstract

The invention discloses a multi-micro-nano satellite rapid deployment structure for on-orbit service of non-cooperative targets, which belongs to the field of aerospace. The structure includes a regular dodecahedron frame, and each edge of the regular dodecahedron frame The hook assembly is installed on the top; micro-nano satellites are arranged on the twelve faces of the regular dodecahedron frame, and the top of the micro-nano satellites is a regular five-sided pyramid structure, and the regular five-sided Inside the dihedral frame, the top outer surface of the micro-nano-satellite body is aligned with the dodecahedron frame, and the micro-nano-satellite body is fixed or released by hook assembly; the structure of the present invention can adapt to various The launch position and direction can be adaptively adjusted to the space attitude, and the hook structure on the frame can be used to quickly fix and release the micro-nano satellite. And deploy multi-micro-nano satellites.

Description

technical field [0001] The invention belongs to the field of aerospace, in particular to a multi-micro-nano satellite rapid deployment structure for on-orbit service of non-cooperative targets. Background technique [0002] The environment of low-Earth orbit space is becoming more and more complex, and the number of space non-cooperative targets including invalid satellites and space debris is increasing, which poses active and passive security threats to active satellites, space stations, spacecraft and other space assets. Realizing on-orbit services for space non-cooperative targets, including rendezvous, capture, and de-orbit operations, is an inevitable trend to achieve space security. However, the traditional on-orbit service tasks relying on a single large satellite to achieve non-cooperative space targets are too costly and insufficient in flexibility. With the gradual maturity of micro-nano-satellite technology, relying on the large-scale cluster effect of micro-nan...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G4/00
CPCB64G4/00
Inventor 龚柏春张子昊秦远田薛双全
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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