Dynamic models of satellite relative motion around an oblate earth

Danwei Wang; Baolin Wu; Eng Kee Poh

doi:10.1007/978-981-10-2383-5_2

Dynamic models of satellite relative motion around an oblate earth

Danwei Wang^*
, Baolin Wu
, Eng Kee Poh

^*Corresponding author for this work

School of Astronautics

Nanyang Technological University

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

11 Scopus citations

Abstract

Accurate dynamic model of relative motion is basic and critical to the study of satellite formation flying. So accurate nonlinear and linear dynamic models of satellite relative motion considering J² perturbation are derived in this chapter.

Original language	English
Title of host publication	Intelligent Systems, Control and Automation
Subtitle of host publication	Science and Engineering
Publisher	Kluwer Academic Publishers
Pages	9-41
Number of pages	33
DOIs	https://doi.org/10.1007/978-981-10-2383-5_2
State	Published - 1 Oct 2017

Publication series

Name	Intelligent Systems, Control and Automation: Science and Engineering
Volume	87
ISSN (Print)	2213-8986
ISSN (Electronic)	2213-8994

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10.1007/978-981-10-2383-5_2

Cite this

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title = "Dynamic models of satellite relative motion around an oblate earth",

abstract = "Accurate dynamic model of relative motion is basic and critical to the study of satellite formation flying. So accurate nonlinear and linear dynamic models of satellite relative motion considering J2 perturbation are derived in this chapter.",

author = "Danwei Wang and Baolin Wu and Poh, \{Eng Kee\}",

note = "Publisher Copyright: {\textcopyright} Springer Science+Business Media Singapore 2017.",

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Dynamic models of satellite relative motion around an oblate earth. / Wang, Danwei; Wu, Baolin; Poh, Eng Kee.
Intelligent Systems, Control and Automation: Science and Engineering. Kluwer Academic Publishers, 2017. p. 9-41 (Intelligent Systems, Control and Automation: Science and Engineering; Vol. 87).

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

TY - CHAP

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AU - Wu, Baolin

AU - Poh, Eng Kee

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N2 - Accurate dynamic model of relative motion is basic and critical to the study of satellite formation flying. So accurate nonlinear and linear dynamic models of satellite relative motion considering J2 perturbation are derived in this chapter.

AB - Accurate dynamic model of relative motion is basic and critical to the study of satellite formation flying. So accurate nonlinear and linear dynamic models of satellite relative motion considering J2 perturbation are derived in this chapter.

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M3 - 章节

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ER -

Dynamic models of satellite relative motion around an oblate earth

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