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

High-precision spacecraft radiation light pressure modeling method

A modeling method and spacecraft technology, applied in the aerospace field, can solve the problems of long calculation time, difficult to meet the needs of rapid and high-precision radiation optical pressure modeling of massive spacecraft, and large amount of calculation, so as to achieve easy calculation and management, Strong applicability and the effect of improving calculation speed

Pending Publication Date: 2021-12-03
BEIHANG UNIV
View PDF0 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the above two methods have the disadvantages of large amount of calculation and long calculation time, and it is difficult to meet the fast and high-precision radiation light pressure modeling requirements of massive spacecraft.

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
  • High-precision spacecraft radiation light pressure modeling method
  • High-precision spacecraft radiation light pressure modeling method
  • High-precision spacecraft radiation light pressure modeling method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0076] Taking the JASON-2 marine altimetry satellite as an example, the high-precision spacecraft radiation light pressure modeling method provided by the present invention is described, which specifically includes the following steps:

[0077] S1: According to the position of the satellite and the sun in the inertial system, calculate the solar radiation reaching the satellite position, as well as the earth's short-wave radiation and long-wave radiation; the long-wave radiation and short-wave radiation should be calculated separately, figure 2 Shows the process of calculating longwave radiation and shortwave radiation on a triangular grid on the earth's surface, where shortwave radiation can only reach the satellite when the triangular grid is visible to both the satellite and the spacecraft, and longwave radiation can only be seen as long as the triangular grid is visible to the satellite satellites can be reached.

[0078] S2: To construct a 3D database according to the ac...

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 high-precision spacecraft radiation light pressure modeling method. According to the method, unified modeling is conducted on solar radiation pressure, earth radiation pressure and thermal radiation light pressure borne by a spacecraft. A three-dimensional structure of the spacecraft is finely represented by using a geometric prototype, the characteristic parameters of a surface material are given, and a three-dimensional model database of the spacecraft is constructed. A ray tracing method is used to simulate the interaction between radiation and the surface of the spacecraft to obtain the radiation light pressure acceleration expressed in a spacecraft body system, and therefore a radiation light pressure model of the spacecraft is established. The solar radiation pressure, the earth radiation pressure, the thermal radiation pressure and the uncertainty are output in the form of grids. A user only needs to execute simple bilinear interpolation on the basis of a grid file to obtain the high-precision radiation light pressure acceleration of the spacecraft in any attitude. As a high-precision non-conservative force modeling method, the method can perfect and improve the orbit dynamics model of the spacecraft, and further improve the orbit determination precision and the orbit prediction accuracy.

Description

technical field [0001] The invention belongs to the field of aerospace, in particular to a high-precision spacecraft radiation light pressure modeling method. Background technique [0002] Radiation light pressure, as a non-conservative force, is a mechanical effect produced by the momentum transfer when photons collide with the surface of an object. For Earth-orbiting spacecraft, the flow of radiation photons from the Sun, the Earth, and the spacecraft itself interacts with the surface of the spacecraft, creating radiation light pressure. Although the magnitude of the radiation light pressure is small, it will have a large impact on the orbit of the long-term orbiting spacecraft. Compared with the earth's gravity and the sun's and moon's gravity, which have relatively mature modeling technology and high precision, due to the influence of factors such as changes in radiation intensity, deviations in spacecraft attitude control, and aging of surface materials, the high-accur...

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): G06F30/15G06F30/20G06F119/08
CPCG06F30/15G06F30/20G06F2119/08Y02E60/00
Inventor 李桢施闯肖云潘宗鹏张雨露
Owner BEIHANG 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