Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Space-air-ground two-dimensional pointing mechanism for low Earth orbit (LEO) or medium Earth orbit (MEO) spacecraft, and tracking method implemented by pointing mechanism

A pointing mechanism and spacecraft technology, applied in the direction of attitude control, etc., can solve the problem of simplification of the functions of the two-dimensional pointing mechanism, and achieve the effect of flexible use, simple use, and favorable layout of the whole star

Active Publication Date: 2019-08-20
SHANGHAI SATELLITE ENG INST
View PDF7 Cites 3 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] Aiming at the defects of the prior art, the object of the present invention is to provide a space-ground two-dimensional pointing mechanism for a medium-low orbit spacecraft and its tracking method, which overcomes the oversimplification of the functions of the two-dimensional pointing mechanism of the existing spacecraft and the need for multiple pairs of different functions. Insufficiency of two-dimensional pointing mechanism

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Space-air-ground two-dimensional pointing mechanism for low Earth orbit (LEO) or medium Earth orbit (MEO) spacecraft, and tracking method implemented by pointing mechanism
  • Space-air-ground two-dimensional pointing mechanism for low Earth orbit (LEO) or medium Earth orbit (MEO) spacecraft, and tracking method implemented by pointing mechanism
  • Space-air-ground two-dimensional pointing mechanism for low Earth orbit (LEO) or medium Earth orbit (MEO) spacecraft, and tracking method implemented by pointing mechanism

Examples

Experimental program
Comparison scheme
Effect test

Embodiment

[0041]In the present embodiment, the sky-ground two-dimensional pointing mechanism of the medium and low orbit spacecraft of the present invention is introduced as follows: it includes an electric control box, a two-dimensional pointing mechanism with a pair of drive shafts orthogonal to it, and a two-dimensional pointing mechanism for installing the two-dimensional pointing mechanism. Pointing to the platform, the two rotatable angles of the pointing mechanism are greater than 300 degrees, and the base of the mechanism can be positioned at the X position of the spacecraft. b direction, and can also be in the Y b direction.

[0042] Next, the present invention will be described in detail.

[0043] The object of the present invention is to provide a space-ground two-dimensional pointing mechanism for a medium-low orbit spacecraft and its tracking method, which overcomes the problem that the existing spacecraft two-dimensional pointing mechanism has a single function and needs ...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention belongs to the technical field of overall spacecraft designing, and relates to a space-air-ground two-dimensional pointing mechanism for a low Earth orbit (LEO) or medium Earth orbit (MEO) spacecraft. The space-air-ground two-dimensional pointing mechanism comprises an electric control box, a two-dimensional pointing mechanism with orthogonal driving shafts, and a pointing platform used for installation of the two-dimensional pointing mechanism, wherein the pointing mechanism is provided with two rotation angles; and a base of the mechanism can be arranged in an Xb direction or aYb direction of the spacecraft. The space-air-ground two-dimensional pointing mechanism provided by the invention has the advantages that space pointing, air pointing and ground pointing of the LEO or MEO spacecraft can be completed, that is, pointing of the LEO or MEO spacecraft to a relay satellite, other LEO or MEO spacecrafts and a ground station can be completed, only through the single two-dimensional pointing mechanism, so that the spacecraft integration level can be greatly improved, the spacecraft size can be reduced, and the spacecraft cost can be lowered; and the pointing mechanismcan be flexibly used and can be provided with multiple pointing correction measures, so that the characteristics of high pointing precision and high simplicity in use can be achieved.

Description

technical field [0001] The invention relates to the technical field of overall design of spacecraft, in particular to a space-ground two-dimensional pointing mechanism and a tracking method for a medium-low orbit spacecraft. Background technique [0002] With the development of high-resolution remote sensing technology, the on-orbit data code rate of spacecraft is getting higher and higher. More and more spacecraft on-orbit data transmission schemes use point-beam antennas or laser communication and other pointing data transmission schemes. The instrument has a two-dimensional pointing mechanism for tracking the pointing of the ground station. [0003] Secondly, the time for medium and low orbit spacecraft to pass over the domestic ground station is very short every day. For the territory of our country, it can generally fly over 4 orbits in the territory every day, and each orbit usually only takes about 10 minutes. Under the limited data transmission code rate, the effecti...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/08
Inventor 温渊杨勇邵益凯李云端蒋光伟孙允珠
Owner SHANGHAI SATELLITE ENG INST
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products