Attitude Tracking Control of Reusable Launch Vehicle During Deceleration Phase Based on Periodic Delayed Sliding Mode Surface

Junjie Sha; Zhao Yan Li; Mengyang Wang

doi:10.1109/CCDC69976.2026.11559926

Attitude Tracking Control of Reusable Launch Vehicle During Deceleration Phase Based on Periodic Delayed Sliding Mode Surface

Junjie Sha
, Zhao Yan Li^*
, Mengyang Wang

^*Corresponding author for this work

School of Mathematics

Harbin Institute of Technology
Zhengzhou Research Institute of HIT

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

Abstract

This paper proposes a prescribed-time control method based on a periodic delayed mode surface under strong disturbance to track the attitude of reusable vehicle during deceleration phase. Firstly, a three-dimensional launch vehicle kinematic model is established. Secondly, based on a secondorder chained integral structure, a spatial attitude control system model is constructed. Finally, a prescribed-time extended state observer (PTESO) with periodic-delay feedback is designed to effectively estimate and compensate for strong disturbances. Simulation validate the correctness of theoretical derivations and the effectiveness of the control strategy.

Original language	English
Title of host publication	38th Chinese Control and Decision Conference, CCDC 2026
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	6105-6110
Number of pages	6
ISBN (Electronic)	9798331550707
DOIs	https://doi.org/10.1109/CCDC69976.2026.11559926
State	Published - 2026
Event	38th Chinese Control and Decision Conference, CCDC 2026 - Nanjing, China Duration: 15 May 2026 → 18 May 2026

Publication series

Name	38th Chinese Control and Decision Conference, CCDC 2026

Conference

Conference	38th Chinese Control and Decision Conference, CCDC 2026
Country/Territory	China
City	Nanjing
Period	15/05/26 → 18/05/26

Keywords

Periodic delayed sliding mode surface
Prescribed-time extended state observer
Vehicle re-entry

Access to Document

10.1109/CCDC69976.2026.11559926

Cite this

Sha, J., Li, Z. Y., & Wang, M. (2026). Attitude Tracking Control of Reusable Launch Vehicle During Deceleration Phase Based on Periodic Delayed Sliding Mode Surface. In 38th Chinese Control and Decision Conference, CCDC 2026 (pp. 6105-6110). (38th Chinese Control and Decision Conference, CCDC 2026). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CCDC69976.2026.11559926

@inproceedings{ea1bea423cb04047908a294b20eb8f5e,

title = "Attitude Tracking Control of Reusable Launch Vehicle During Deceleration Phase Based on Periodic Delayed Sliding Mode Surface",

abstract = "This paper proposes a prescribed-time control method based on a periodic delayed mode surface under strong disturbance to track the attitude of reusable vehicle during deceleration phase. Firstly, a three-dimensional launch vehicle kinematic model is established. Secondly, based on a secondorder chained integral structure, a spatial attitude control system model is constructed. Finally, a prescribed-time extended state observer (PTESO) with periodic-delay feedback is designed to effectively estimate and compensate for strong disturbances. Simulation validate the correctness of theoretical derivations and the effectiveness of the control strategy.",

keywords = "Periodic delayed sliding mode surface, Prescribed-time extended state observer, Vehicle re-entry",

author = "Junjie Sha and Li, \{Zhao Yan\} and Mengyang Wang",

note = "Publisher Copyright: {\textcopyright} 2026 IEEE.; 38th Chinese Control and Decision Conference, CCDC 2026 ; Conference date: 15-05-2026 Through 18-05-2026",

year = "2026",

doi = "10.1109/CCDC69976.2026.11559926",

language = "英语",

series = "38th Chinese Control and Decision Conference, CCDC 2026",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

pages = "6105--6110",

booktitle = "38th Chinese Control and Decision Conference, CCDC 2026",

address = "美国",

}

Sha, J, Li, ZY & Wang, M 2026, Attitude Tracking Control of Reusable Launch Vehicle During Deceleration Phase Based on Periodic Delayed Sliding Mode Surface. in 38th Chinese Control and Decision Conference, CCDC 2026. 38th Chinese Control and Decision Conference, CCDC 2026, Institute of Electrical and Electronics Engineers Inc., pp. 6105-6110, 38th Chinese Control and Decision Conference, CCDC 2026, Nanjing, China, 15/05/26. https://doi.org/10.1109/CCDC69976.2026.11559926

Attitude Tracking Control of Reusable Launch Vehicle During Deceleration Phase Based on Periodic Delayed Sliding Mode Surface. / Sha, Junjie; Li, Zhao Yan; Wang, Mengyang.
38th Chinese Control and Decision Conference, CCDC 2026. Institute of Electrical and Electronics Engineers Inc., 2026. p. 6105-6110 (38th Chinese Control and Decision Conference, CCDC 2026).

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

TY - GEN

T1 - Attitude Tracking Control of Reusable Launch Vehicle During Deceleration Phase Based on Periodic Delayed Sliding Mode Surface

AU - Sha, Junjie

AU - Li, Zhao Yan

AU - Wang, Mengyang

PY - 2026

Y1 - 2026

N2 - This paper proposes a prescribed-time control method based on a periodic delayed mode surface under strong disturbance to track the attitude of reusable vehicle during deceleration phase. Firstly, a three-dimensional launch vehicle kinematic model is established. Secondly, based on a secondorder chained integral structure, a spatial attitude control system model is constructed. Finally, a prescribed-time extended state observer (PTESO) with periodic-delay feedback is designed to effectively estimate and compensate for strong disturbances. Simulation validate the correctness of theoretical derivations and the effectiveness of the control strategy.

AB - This paper proposes a prescribed-time control method based on a periodic delayed mode surface under strong disturbance to track the attitude of reusable vehicle during deceleration phase. Firstly, a three-dimensional launch vehicle kinematic model is established. Secondly, based on a secondorder chained integral structure, a spatial attitude control system model is constructed. Finally, a prescribed-time extended state observer (PTESO) with periodic-delay feedback is designed to effectively estimate and compensate for strong disturbances. Simulation validate the correctness of theoretical derivations and the effectiveness of the control strategy.

KW - Periodic delayed sliding mode surface

KW - Prescribed-time extended state observer

KW - Vehicle re-entry

UR - https://www.scopus.com/pages/publications/105043951155

U2 - 10.1109/CCDC69976.2026.11559926

DO - 10.1109/CCDC69976.2026.11559926

M3 - 会议稿件

AN - SCOPUS:105043951155

T3 - 38th Chinese Control and Decision Conference, CCDC 2026

SP - 6105

EP - 6110

BT - 38th Chinese Control and Decision Conference, CCDC 2026

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 38th Chinese Control and Decision Conference, CCDC 2026

Y2 - 15 May 2026 through 18 May 2026

ER -

Sha J, Li ZY, Wang M. Attitude Tracking Control of Reusable Launch Vehicle During Deceleration Phase Based on Periodic Delayed Sliding Mode Surface. In 38th Chinese Control and Decision Conference, CCDC 2026. Institute of Electrical and Electronics Engineers Inc. 2026. p. 6105-6110. (38th Chinese Control and Decision Conference, CCDC 2026). doi: 10.1109/CCDC69976.2026.11559926

Attitude Tracking Control of Reusable Launch Vehicle During Deceleration Phase Based on Periodic Delayed Sliding Mode Surface

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