2006Journal of Zhengzhou Institute of Surveying and MappingRequires access

Global Navigation Satellite Constellation Design Using Walker Constellation

Fuping Sun

Open publisher page 9 citations

Abstract

The effects of the orbital plane number,satellite number and orbital eccentricity on constellation capabilities are discussed.Through the comparative calculations on three kinds of configuration,six kinds of semi major axis and orbital inclination between 46°~66°,the original configurations are designed based on the constellation CV values in repeat period.Combined with the coverage capability,the most DOP value and precision usability,the global navigation satellite constellation using Walker-δ constellation is introduced.The method of strengthen the local navigation capability is discussed by adding the GEO satellite.

About this research paper

What this paper is about

The effects of the orbital plane number,satellite number and orbital eccentricity on constellation capabilities are discussed.Through the comparative calculations on three kinds of configuration,six kinds of semi major axis and orbital inclination between 46°~66°,the original configurations are designed based on the constellation CV values in repeat period.Combined with the coverage capability,the most DOP value and precision usability,the global navigation satellite constellation using Walker-δ constellation is introduced.The method of strengthen the local navigation capability is discussed by adding the GEO satellite.

Why it matters

OpenAlex reports 9 citations for this work. Citation counts describe recorded attention and do not establish research quality.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

The effects of the orbital plane number,satellite number and orbital eccentricity on constellation capabilities are discussed.Through the comparative calculations on three kinds of configuration,six kinds of semi major axis and orbital inclination between 46°~66°,the original configurations are designed based on the constellation CV values in repeat period.Combined with the coverage capability,the most DOP value and precision usability,the global navigation satellite constellation using Walker-δ constellation is introduced.The method of strengthen the local navigation capability is discussed by adding the GEO satellite.

Key concepts: Constellation, Satellite constellation, Computer science, Satellite, Orbital elements, Satellite navigation, Orbital plane, Remote sensing

Related papers

Back to paper searchBrowse research topicsOriginal source
Global Navigation Satellite Constellation Design Using Walker Constellation — Research Paper | ScholarLens