Spacecraft heliocentric ellipse suspension track design method based on solar sail propulsion technology
A technology of heliocentric ellipse and design method, which is applied in the aerospace field and can solve the problem that such orbits are difficult to achieve.
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0052] Aiming at the task of real-time observation of the polar regions of celestial bodies in elliptical Kepler motion around the sun, the present invention proposes a general design method for spacecraft heliocentric elliptical suspension orbits based on solar sail propulsion technology.
[0053] In order to achieve the above object, the implementation method of the present invention is as follows: a design method of a spacecraft heliocentric elliptical suspension orbit based on solar sail propulsion technology is designed. First, according to the mission requirements, the characteristic analysis and decomposition of the levitation height of the heliocentric elliptical levitation orbit are carried out. On this basis, a new rotating non-consistent coordinate system is defined, and the spacecraft dynamics model is established in this coordinate system. Then the parameters of the solar sail to realize the elliptical levitation orbit of the spacecraft are obtained. The detailed ...
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