Modified Two-Dimensional Coverage Analysis Method Considering Various Perturbations

Shengzhou Bai; Yujin Zhang; Yiping Jiang; Wei Sun; Wenjia Shao

doi:10.1109/TAES.2023.3348423

Modified Two-Dimensional Coverage Analysis Method Considering Various Perturbations

Shengzhou Bai
, Yujin Zhang
, Yiping Jiang
, Wei Sun
, Wenjia Shao

The Hong Kong Polytechnic University

Research output: Journal article publication › Journal article › Academic research › peer-review

11 Citations (Scopus)

Abstract

This article proposes a modified 2-D coverage method for satellite coverage analysis considering various perturbations. First, the basic mathematical model, including the standard 2-D field-mapping method and frequently used perturbation model, is introduced. Then, based on the osculating orbital elements, a modified 2-D field-mapping method is presented for calculating visible intervals between a satellite and a target accurately and efficiently. Furthermore, based on the analytical partial differential of the field-element equations with respect to the orbital elements, the maximum error of the proposed method is calculated to estimate its accuracy. The simulation results demonstrate that the proposed method is accurate and effective, indicating its wide application prospect in coverage analysis involving various perturbations.

Original language	English
Pages (from-to)	2763-2777
Number of pages	15
Journal	IEEE Transactions on Aerospace and Electronic Systems
Volume	60
Issue number	3
DOIs	https://doi.org/10.1109/TAES.2023.3348423
Publication status	Published - 1 Jun 2024

Keywords

2-D map
Field-element equations
orbital perturbation
Visibility

ASJC Scopus subject areas

Aerospace Engineering
Electrical and Electronic Engineering

More information

10.1109/TAES.2023.3348423

Cite this

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title = "Modified Two-Dimensional Coverage Analysis Method Considering Various Perturbations",

abstract = "This article proposes a modified 2-D coverage method for satellite coverage analysis considering various perturbations. First, the basic mathematical model, including the standard 2-D field-mapping method and frequently used perturbation model, is introduced. Then, based on the osculating orbital elements, a modified 2-D field-mapping method is presented for calculating visible intervals between a satellite and a target accurately and efficiently. Furthermore, based on the analytical partial differential of the field-element equations with respect to the orbital elements, the maximum error of the proposed method is calculated to estimate its accuracy. The simulation results demonstrate that the proposed method is accurate and effective, indicating its wide application prospect in coverage analysis involving various perturbations.",

keywords = "2-D map, Field-element equations, orbital perturbation, Visibility",

author = "Shengzhou Bai and Yujin Zhang and Yiping Jiang and Wei Sun and Wenjia Shao",

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T1 - Modified Two-Dimensional Coverage Analysis Method Considering Various Perturbations

AU - Bai, Shengzhou

AU - Zhang, Yujin

AU - Jiang, Yiping

AU - Sun, Wei

AU - Shao, Wenjia

PY - 2024/6/1

Y1 - 2024/6/1

N2 - This article proposes a modified 2-D coverage method for satellite coverage analysis considering various perturbations. First, the basic mathematical model, including the standard 2-D field-mapping method and frequently used perturbation model, is introduced. Then, based on the osculating orbital elements, a modified 2-D field-mapping method is presented for calculating visible intervals between a satellite and a target accurately and efficiently. Furthermore, based on the analytical partial differential of the field-element equations with respect to the orbital elements, the maximum error of the proposed method is calculated to estimate its accuracy. The simulation results demonstrate that the proposed method is accurate and effective, indicating its wide application prospect in coverage analysis involving various perturbations.

AB - This article proposes a modified 2-D coverage method for satellite coverage analysis considering various perturbations. First, the basic mathematical model, including the standard 2-D field-mapping method and frequently used perturbation model, is introduced. Then, based on the osculating orbital elements, a modified 2-D field-mapping method is presented for calculating visible intervals between a satellite and a target accurately and efficiently. Furthermore, based on the analytical partial differential of the field-element equations with respect to the orbital elements, the maximum error of the proposed method is calculated to estimate its accuracy. The simulation results demonstrate that the proposed method is accurate and effective, indicating its wide application prospect in coverage analysis involving various perturbations.

KW - 2-D map

KW - Field-element equations

KW - orbital perturbation

KW - Visibility

UR - https://www.scopus.com/pages/publications/85181558893

U2 - 10.1109/TAES.2023.3348423

DO - 10.1109/TAES.2023.3348423

M3 - Journal article

AN - SCOPUS:85181558893

SN - 0018-9251

VL - 60

SP - 2763

EP - 2777

JO - IEEE Transactions on Aerospace and Electronic Systems

JF - IEEE Transactions on Aerospace and Electronic Systems

IS - 3

ER -

Modified Two-Dimensional Coverage Analysis Method Considering Various Perturbations

Abstract

Keywords

ASJC Scopus subject areas

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