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

Satellite optical camouflage method

A satellite and optical technology, applied in the field of computing, can solve the problems of passive stealth process and great influence on mission functions, and achieve the effect of improving concealment and security

Inactive Publication Date: 2019-07-12
PLA PEOPLES LIBERATION ARMY OF CHINA STRATEGIC SUPPORT FORCE AEROSPACE ENG UNIV
View PDF5 Cites 3 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Due to the particularity of the satellite’s in-orbit space operating environment and the limitations of the types of materials commonly used on the surface of space targets, the research on optical stealth satellites at home and abroad starts with the target’s macrostructure, which makes the mission function of the satellite itself greatly affected by the satellite’s stealth design. The design needs to redesign the matching platform type, and the macro stealth design is formed at one time, the stealth process is still relatively passive, and it cannot be actively adjusted according to the actual task to achieve intelligent "transformation"

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
  • Satellite optical camouflage method
  • Satellite optical camouflage method
  • Satellite optical camouflage method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0051] Embodiment 1 of the present invention provides a method for satellite optical camouflage provided by the present invention, the method comprising:

[0052] Step 1. Receive a customized task that requires the photometric curve presented by the satellite within the observation arc.

[0053] The photometric curves that need to be presented by the satellite in the customized task include photometric curves of different shapes, different attitudes, different stable states, and different working states.

[0054]Different stable states, shapes, postures and working states of space objects have different shapes of their photometric curves. Customize the shape of photometric curves so that the photometric curves obtained from the perspective of the detector show the unreal characteristics of space objects, so as to achieve The purpose of optical "transformation". That is to say, the customization of the shape of the photometric curve can be realized by customizing the character...

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 discloses a satellite optical camouflage method. The satellite optical camouflage method comprises the steps that a customizing task of a luminosity curve needing a satellite to displayin an observation segmental arc is received; positions of the sun and a detector in a satellite centroid orbit coordinate system in the observation segmental arc is resolved and calculated; the direction of an angular bisector of a sun position vector and a detector position vector in the observation segmental arc is resolved and calculated; the number of normal directions of surface panel sand needing to turn to the direction of the angular bisector of the sun position vector and the detector position vector at the time in the observation segmental arc at all time is determined, wherein the surface panels are installed on the surface of the satellite; and a determined number of the surface panels are turned to the direction of the angular bisector of the sun position vector and the detector position vector, and the normal directions of a rest number of the surface panels are made to deviate from the direction by more than 30 degrees. According to the satellite optical camouflage method, the problem that a high orbit satellite avoids ground optical monitoring is solved, by covering the satellite surface with special secular reflection characteristic material surface panels, the reflection direction of the surface panels is controlled, and simulation on the detection of the customized detector for the luminosity curve of a target is achieved.

Description

technical field [0001] The invention relates to a method for satellite optical camouflage, which belongs to the computing field. Background technique [0002] Satellite stealth is to take technical measures to reduce the monitoring possibility of satellite microwave, infrared, and visible light detection equipment in response to the detection threats faced by satellites in orbit. The purpose of satellites in orbit is difficult to be found, difficult to be hit, and difficult to be destroyed. [0003] Optical stealth is mainly divided into two types: material stealth and shape stealth. Material stealth is to reduce the probability of detection by using infrared control material or visible light reflection control material, so as to realize satellite stealth; shape stealth design is to change its structural characteristics so that Monitoring equipment mistook it for space junk or debris, etc. [0004] Due to the particularity of the satellite’s in-orbit space operating enviro...

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
IPC IPC(8): B64G1/52
CPCB64G1/52
Inventor 张峰李智徐灿张雅声霍俞蓉方宇强汉京滨周驰谢杨峻
Owner PLA PEOPLES LIBERATION ARMY OF CHINA STRATEGIC SUPPORT FORCE AEROSPACE ENG UNIV
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