A satellite constellation implementation method using return orbit to implement communication
A technology of satellite constellation and return to orbit, applied in the field of satellite communication, can solve the problem of high difficulty, and achieve the effect of reducing the difficulty of coordination, reducing co-channel interference, and avoiding co-channel interference
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0016] The present invention will be described in detail below with reference to the drawings and embodiments.
[0017] The present invention provides a method for implementing a satellite constellation for communication using a regression orbit, which includes the following steps:
[0018] 1) Determine the regression period and the semi-major axis of the orbit, as well as the inclination of the orbit, the eccentricity of the orbit and the argument of perigee;
[0019] Among them, according to the width of the satellite coverage strip and communication delay requirements, determine the regression period and the semi-major axis of the orbit in a preset set; determine the orbit inclination according to the latitude distribution of the coverage area, so that the orbit inclination is not lower than the coverage The geocentric angle corresponding to the half beam width is subtracted from the highest latitude of the area; the eccentricity and argument of perigee of the orbit are determined...
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