Method for determining deep space detector equivalent transfer orbit
A technology for deep space detectors and transfer orbits, which is applied in the direction of instruments, measuring devices, surveying and navigation, etc., and can solve the problems of no introduction
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment
[0077] The "Kuafu" program is an international cooperation project aimed at solar-terrestrial space weather detection and forecasting. The mission orbit of the "Kuafu-A" star is a halo orbit around the L1 point of the sun and the earth, and the distance between the orbit and the earth is not less than 1.27 million kilometers. The "Kuafu A" star is directly sent by rocket into a transfer orbit with a perigee altitude of 200 kilometers and an apogee of 1.27 million kilometers. The "Kuafu A" star is not only affected by the gravitational force of the earth, but also by the gravitational force of the larger moon and the sun in the transfer orbit. The space mechanics environment is complicated, and its orbital shape is no longer a simple ellipse, such as image 3 shown; image 3 Shown in is the projection of the precise transfer orbit in the ecliptic plane (the reference coordinate system is the geocentric ecliptic rotation coordinate system), so it can be seen that this is a space...
PUM
Abstract
Description
Claims
Application Information
- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com