Mars Ascent Vehicle Tracking Guidance Law Design Added by Sliding Mode Control in the Coasting Phase

Kun Li; Minwen Guo; Guangfu Ma; Hui Zhi; Yanning Guo

doi:10.23919/CCC52363.2021.9549776

Mars Ascent Vehicle Tracking Guidance Law Design Added by Sliding Mode Control in the Coasting Phase

Kun Li
, Minwen Guo
, Guangfu Ma
, Hui Zhi
, Yanning Guo

School of Astronautics

Harbin Institute of Technology
CAS - Beijing Institute of Control Engineering

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

1 Scopus citations

Abstract

This paper studies the design of the guidance law for the nominal trajectory tracking of the Mars ascent vehicle. First of all, the nominal trajectory of the flight process is optimized according to the needs of the mission. Secondly, for the ascending phase, the speed loss caused by the atmosphere in the coasting phase is considered, and the altitude and speed at the apoapsis are corrected. The vehicle is guided by the closed-loop control of the angle of attack and the angle of sideslip. In addition, for the problem of large trajectory tracking error caused by guidance only in the ascending phase, the sliding mode guidance law of the coasting phase is designed. Finally, through numerical simulation, it is verified that the designed guidance law can improve the tracking accuracy and greatly reduce the fuel consumption required for the rounding into orbit.

Original language	English
Title of host publication	Proceedings of the 40th Chinese Control Conference, CCC 2021
Editors	Chen Peng, Jian Sun
Publisher	IEEE Computer Society
Pages	3541-3546
Number of pages	6
ISBN (Electronic)	9789881563804
DOIs	https://doi.org/10.23919/CCC52363.2021.9549776
State	Published - 26 Jul 2021
Event	40th Chinese Control Conference, CCC 2021 - Shanghai, China Duration: 26 Jul 2021 → 28 Jul 2021

Publication series

Name	Chinese Control Conference, CCC
Volume	2021-July
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	40th Chinese Control Conference, CCC 2021
Country/Territory	China
City	Shanghai
Period	26/07/21 → 28/07/21

Keywords

Coasting Phase Guidance
Mars Ascent Vehicle
Sliding Mode Control
Tracking Guidance

Access to Document

10.23919/CCC52363.2021.9549776

Cite this

Li, K., Guo, M., Ma, G., Zhi, H., & Guo, Y. (2021). Mars Ascent Vehicle Tracking Guidance Law Design Added by Sliding Mode Control in the Coasting Phase. In C. Peng, & J. Sun (Eds.), Proceedings of the 40th Chinese Control Conference, CCC 2021 (pp. 3541-3546). (Chinese Control Conference, CCC; Vol. 2021-July). IEEE Computer Society. https://doi.org/10.23919/CCC52363.2021.9549776

@inproceedings{da39f9fe3f2f4020a1e31e6dcc7c4132,

title = "Mars Ascent Vehicle Tracking Guidance Law Design Added by Sliding Mode Control in the Coasting Phase",

abstract = "This paper studies the design of the guidance law for the nominal trajectory tracking of the Mars ascent vehicle. First of all, the nominal trajectory of the flight process is optimized according to the needs of the mission. Secondly, for the ascending phase, the speed loss caused by the atmosphere in the coasting phase is considered, and the altitude and speed at the apoapsis are corrected. The vehicle is guided by the closed-loop control of the angle of attack and the angle of sideslip. In addition, for the problem of large trajectory tracking error caused by guidance only in the ascending phase, the sliding mode guidance law of the coasting phase is designed. Finally, through numerical simulation, it is verified that the designed guidance law can improve the tracking accuracy and greatly reduce the fuel consumption required for the rounding into orbit.",

keywords = "Coasting Phase Guidance, Mars Ascent Vehicle, Sliding Mode Control, Tracking Guidance",

author = "Kun Li and Minwen Guo and Guangfu Ma and Hui Zhi and Yanning Guo",

note = "Publisher Copyright: {\textcopyright} 2021 Technical Committee on Control Theory, Chinese Association of Automation.; 40th Chinese Control Conference, CCC 2021 ; Conference date: 26-07-2021 Through 28-07-2021",

year = "2021",

month = jul,

day = "26",

doi = "10.23919/CCC52363.2021.9549776",

language = "英语",

series = "Chinese Control Conference, CCC",

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editor = "Chen Peng and Jian Sun",

booktitle = "Proceedings of the 40th Chinese Control Conference, CCC 2021",

address = "美国",

}

Li, K, Guo, M, Ma, G, Zhi, H & Guo, Y 2021, Mars Ascent Vehicle Tracking Guidance Law Design Added by Sliding Mode Control in the Coasting Phase. in C Peng & J Sun (eds), Proceedings of the 40th Chinese Control Conference, CCC 2021. Chinese Control Conference, CCC, vol. 2021-July, IEEE Computer Society, pp. 3541-3546, 40th Chinese Control Conference, CCC 2021, Shanghai, China, 26/07/21. https://doi.org/10.23919/CCC52363.2021.9549776

Mars Ascent Vehicle Tracking Guidance Law Design Added by Sliding Mode Control in the Coasting Phase. / Li, Kun; Guo, Minwen; Ma, Guangfu et al.
Proceedings of the 40th Chinese Control Conference, CCC 2021. ed. / Chen Peng; Jian Sun. IEEE Computer Society, 2021. p. 3541-3546 (Chinese Control Conference, CCC; Vol. 2021-July).

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

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T1 - Mars Ascent Vehicle Tracking Guidance Law Design Added by Sliding Mode Control in the Coasting Phase

AU - Li, Kun

AU - Guo, Minwen

AU - Ma, Guangfu

AU - Zhi, Hui

AU - Guo, Yanning

PY - 2021/7/26

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N2 - This paper studies the design of the guidance law for the nominal trajectory tracking of the Mars ascent vehicle. First of all, the nominal trajectory of the flight process is optimized according to the needs of the mission. Secondly, for the ascending phase, the speed loss caused by the atmosphere in the coasting phase is considered, and the altitude and speed at the apoapsis are corrected. The vehicle is guided by the closed-loop control of the angle of attack and the angle of sideslip. In addition, for the problem of large trajectory tracking error caused by guidance only in the ascending phase, the sliding mode guidance law of the coasting phase is designed. Finally, through numerical simulation, it is verified that the designed guidance law can improve the tracking accuracy and greatly reduce the fuel consumption required for the rounding into orbit.

AB - This paper studies the design of the guidance law for the nominal trajectory tracking of the Mars ascent vehicle. First of all, the nominal trajectory of the flight process is optimized according to the needs of the mission. Secondly, for the ascending phase, the speed loss caused by the atmosphere in the coasting phase is considered, and the altitude and speed at the apoapsis are corrected. The vehicle is guided by the closed-loop control of the angle of attack and the angle of sideslip. In addition, for the problem of large trajectory tracking error caused by guidance only in the ascending phase, the sliding mode guidance law of the coasting phase is designed. Finally, through numerical simulation, it is verified that the designed guidance law can improve the tracking accuracy and greatly reduce the fuel consumption required for the rounding into orbit.

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KW - Mars Ascent Vehicle

KW - Sliding Mode Control

KW - Tracking Guidance

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ER -

Mars Ascent Vehicle Tracking Guidance Law Design Added by Sliding Mode Control in the Coasting Phase

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