Research on Orbital Maneuver of VLEO Satellite Based on Aerodynamic Assistance

Haoyu Li; Peng Tian; Xiaosong Zhang; Xinbo Xu; Qiaodong Zhang; Hongwei Han

doi:10.1007/978-981-97-7770-9_16

Research on Orbital Maneuver of VLEO Satellite Based on Aerodynamic Assistance

Haoyu Li^*
, Peng Tian
, Xiaosong Zhang
, Xinbo Xu
, Qiaodong Zhang
, Hongwei Han

^*Corresponding author for this work

School of Aerospace Engineering

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

1 Citation (Scopus)

Abstract

In this paper, a very low earth orbit (VLEO) satellite orbit maneuver strategy is designed based on aerodynamic assisted configuration. The effectiveness of the strategy is verified by numerical simulation analysis. The aero-assisted orbital maneuver strategy presented in this paper has the orbit maintenance ability to meet the amplitude tolerance of the mean orbital element oscillation. This research introduced aerodynamic related theory, innovative research in satellite orbit maneuver technology, aerodynamic servo as auxiliary means, effectively reduce the traditional satellite pressure control mechanism. The research results in this paper provide support for the subsequent implementation of high-definition and quick response new system satellites.

Original language	English
Title of host publication	Proceedings of 2024 12th China Conference on Command and Control - Volume I
Publisher	Springer Science and Business Media Deutschland GmbH
Pages	168-182
Number of pages	15
ISBN (Print)	9789819777693
DOIs	https://doi.org/10.1007/978-981-97-7770-9_16
Publication status	Published - 2024
Event	12th China Conference on Command and Control, C2 2024 - Beijing, China Duration: 17 May 2024 → 18 May 2024

Publication series

Name	Lecture Notes in Electrical Engineering
Volume	1266
ISSN (Print)	1876-1100
ISSN (Electronic)	1876-1119

Conference

Conference	12th China Conference on Command and Control, C2 2024
Country/Territory	China
City	Beijing
Period	17/05/24 → 18/05/24

Keywords

Aerodynamic Assistance
Orbital Maneuver
VLEO

Access to Document

10.1007/978-981-97-7770-9_16

Cite this

Li, H., Tian, P., Zhang, X., Xu, X., Zhang, Q., & Han, H. (2024). Research on Orbital Maneuver of VLEO Satellite Based on Aerodynamic Assistance. In Proceedings of 2024 12th China Conference on Command and Control - Volume I (pp. 168-182). (Lecture Notes in Electrical Engineering; Vol. 1266). Springer Science and Business Media Deutschland GmbH. https://doi.org/10.1007/978-981-97-7770-9_16

@inproceedings{aa319965d6ac4838acf9e1cf9a895f81,

title = "Research on Orbital Maneuver of VLEO Satellite Based on Aerodynamic Assistance",

abstract = "In this paper, a very low earth orbit (VLEO) satellite orbit maneuver strategy is designed based on aerodynamic assisted configuration. The effectiveness of the strategy is verified by numerical simulation analysis. The aero-assisted orbital maneuver strategy presented in this paper has the orbit maintenance ability to meet the amplitude tolerance of the mean orbital element oscillation. This research introduced aerodynamic related theory, innovative research in satellite orbit maneuver technology, aerodynamic servo as auxiliary means, effectively reduce the traditional satellite pressure control mechanism. The research results in this paper provide support for the subsequent implementation of high-definition and quick response new system satellites.",

keywords = "Aerodynamic Assistance, Orbital Maneuver, VLEO",

author = "Haoyu Li and Peng Tian and Xiaosong Zhang and Xinbo Xu and Qiaodong Zhang and Hongwei Han",

note = "Publisher Copyright: {\textcopyright} Chinese Institute of Command and Control 2024.; 12th China Conference on Command and Control, C2 2024 ; Conference date: 17-05-2024 Through 18-05-2024",

year = "2024",

doi = "10.1007/978-981-97-7770-9\_16",

language = "English",

isbn = "9789819777693",

series = "Lecture Notes in Electrical Engineering",

publisher = "Springer Science and Business Media Deutschland GmbH",

pages = "168--182",

booktitle = "Proceedings of 2024 12th China Conference on Command and Control - Volume I",

address = "Germany",

}

Li, H, Tian, P, Zhang, X, Xu, X, Zhang, Q & Han, H 2024, Research on Orbital Maneuver of VLEO Satellite Based on Aerodynamic Assistance. in Proceedings of 2024 12th China Conference on Command and Control - Volume I. Lecture Notes in Electrical Engineering, vol. 1266, Springer Science and Business Media Deutschland GmbH, pp. 168-182, 12th China Conference on Command and Control, C2 2024, Beijing, China, 17/05/24. https://doi.org/10.1007/978-981-97-7770-9_16

Research on Orbital Maneuver of VLEO Satellite Based on Aerodynamic Assistance. / Li, Haoyu; Tian, Peng; Zhang, Xiaosong et al.
Proceedings of 2024 12th China Conference on Command and Control - Volume I. Springer Science and Business Media Deutschland GmbH, 2024. p. 168-182 (Lecture Notes in Electrical Engineering; Vol. 1266).

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

TY - GEN

T1 - Research on Orbital Maneuver of VLEO Satellite Based on Aerodynamic Assistance

AU - Li, Haoyu

AU - Tian, Peng

AU - Zhang, Xiaosong

AU - Xu, Xinbo

AU - Zhang, Qiaodong

AU - Han, Hongwei

PY - 2024

Y1 - 2024

N2 - In this paper, a very low earth orbit (VLEO) satellite orbit maneuver strategy is designed based on aerodynamic assisted configuration. The effectiveness of the strategy is verified by numerical simulation analysis. The aero-assisted orbital maneuver strategy presented in this paper has the orbit maintenance ability to meet the amplitude tolerance of the mean orbital element oscillation. This research introduced aerodynamic related theory, innovative research in satellite orbit maneuver technology, aerodynamic servo as auxiliary means, effectively reduce the traditional satellite pressure control mechanism. The research results in this paper provide support for the subsequent implementation of high-definition and quick response new system satellites.

AB - In this paper, a very low earth orbit (VLEO) satellite orbit maneuver strategy is designed based on aerodynamic assisted configuration. The effectiveness of the strategy is verified by numerical simulation analysis. The aero-assisted orbital maneuver strategy presented in this paper has the orbit maintenance ability to meet the amplitude tolerance of the mean orbital element oscillation. This research introduced aerodynamic related theory, innovative research in satellite orbit maneuver technology, aerodynamic servo as auxiliary means, effectively reduce the traditional satellite pressure control mechanism. The research results in this paper provide support for the subsequent implementation of high-definition and quick response new system satellites.

KW - Aerodynamic Assistance

KW - Orbital Maneuver

KW - VLEO

UR - https://www.scopus.com/pages/publications/85218493238

U2 - 10.1007/978-981-97-7770-9_16

DO - 10.1007/978-981-97-7770-9_16

M3 - Conference contribution

AN - SCOPUS:85218493238

SN - 9789819777693

T3 - Lecture Notes in Electrical Engineering

SP - 168

EP - 182

BT - Proceedings of 2024 12th China Conference on Command and Control - Volume I

PB - Springer Science and Business Media Deutschland GmbH

T2 - 12th China Conference on Command and Control, C2 2024

Y2 - 17 May 2024 through 18 May 2024

ER -

Research on Orbital Maneuver of VLEO Satellite Based on Aerodynamic Assistance

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