Finite-time Simultaneous-Arrival-To-Origin Sliding Model Control for Multi-missile Systems

Qiuyu Wang; Pingli Lu; Ye Tian

doi:10.23919/CCC58697.2023.10240566

Finite-time Simultaneous-Arrival-To-Origin Sliding Model Control for Multi-missile Systems

Qiuyu Wang, Pingli Lu^*, Ye Tian

^*Corresponding author for this work

School of Automation

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

1 Citation (Scopus)

Abstract

This paper investigates the problem of multiple missiles attacking a fixed target coordinately. Different from the residual time cooperative control algorithm, direct relative distance control algorithm is designed in this paper. A finite-time simultaneous-arrival-to-origin (SATO) sliding mode control (SMC) algorithm for multi-missile systems (MMSs) is proposed. It is shown that the proposed algorithm can eliminate the singularity problem. Each missile under the algorithm can strike fixed targets simultaneously in finite-time. The stability of proposed algorithm is proved by Lyapunov approach. Besides, simulation results are given to demonstrate the effectiveness of proposed algorithm.

Original language	English
Title of host publication	2023 42nd Chinese Control Conference, CCC 2023
Publisher	IEEE Computer Society
Pages	129-133
Number of pages	5
ISBN (Electronic)	9789887581543
DOIs	https://doi.org/10.23919/CCC58697.2023.10240566
Publication status	Published - 2023
Event	42nd Chinese Control Conference, CCC 2023 - Tianjin, China Duration: 24 Jul 2023 → 26 Jul 2023

Publication series

Name	Chinese Control Conference, CCC
Volume	2023-July
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	42nd Chinese Control Conference, CCC 2023
Country/Territory	China
City	Tianjin
Period	24/07/23 → 26/07/23

Keywords

Finite-time
Multi-missile systems
Simultaneous-arrival-to-origin
Sliding model control

Access to Document

10.23919/CCC58697.2023.10240566

Cite this

@inproceedings{8a38b7623071491c8cf642df8152f710,

title = "Finite-time Simultaneous-Arrival-To-Origin Sliding Model Control for Multi-missile Systems",

abstract = "This paper investigates the problem of multiple missiles attacking a fixed target coordinately. Different from the residual time cooperative control algorithm, direct relative distance control algorithm is designed in this paper. A finite-time simultaneous-arrival-to-origin (SATO) sliding mode control (SMC) algorithm for multi-missile systems (MMSs) is proposed. It is shown that the proposed algorithm can eliminate the singularity problem. Each missile under the algorithm can strike fixed targets simultaneously in finite-time. The stability of proposed algorithm is proved by Lyapunov approach. Besides, simulation results are given to demonstrate the effectiveness of proposed algorithm.",

keywords = "Finite-time, Multi-missile systems, Simultaneous-arrival-to-origin, Sliding model control",

author = "Qiuyu Wang and Pingli Lu and Ye Tian",

note = "Publisher Copyright: {\textcopyright} 2023 Technical Committee on Control Theory, Chinese Association of Automation.; 42nd Chinese Control Conference, CCC 2023 ; Conference date: 24-07-2023 Through 26-07-2023",

year = "2023",

doi = "10.23919/CCC58697.2023.10240566",

language = "English",

series = "Chinese Control Conference, CCC",

publisher = "IEEE Computer Society",

pages = "129--133",

booktitle = "2023 42nd Chinese Control Conference, CCC 2023",

address = "United States",

}

Wang, Q, Lu, P & Tian, Y 2023, Finite-time Simultaneous-Arrival-To-Origin Sliding Model Control for Multi-missile Systems. in 2023 42nd Chinese Control Conference, CCC 2023. Chinese Control Conference, CCC, vol. 2023-July, IEEE Computer Society, pp. 129-133, 42nd Chinese Control Conference, CCC 2023, Tianjin, China, 24/07/23. https://doi.org/10.23919/CCC58697.2023.10240566

Finite-time Simultaneous-Arrival-To-Origin Sliding Model Control for Multi-missile Systems. / Wang, Qiuyu; Lu, Pingli; Tian, Ye.
2023 42nd Chinese Control Conference, CCC 2023. IEEE Computer Society, 2023. p. 129-133 (Chinese Control Conference, CCC; Vol. 2023-July).

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

TY - GEN

T1 - Finite-time Simultaneous-Arrival-To-Origin Sliding Model Control for Multi-missile Systems

AU - Wang, Qiuyu

AU - Lu, Pingli

AU - Tian, Ye

PY - 2023

Y1 - 2023

N2 - This paper investigates the problem of multiple missiles attacking a fixed target coordinately. Different from the residual time cooperative control algorithm, direct relative distance control algorithm is designed in this paper. A finite-time simultaneous-arrival-to-origin (SATO) sliding mode control (SMC) algorithm for multi-missile systems (MMSs) is proposed. It is shown that the proposed algorithm can eliminate the singularity problem. Each missile under the algorithm can strike fixed targets simultaneously in finite-time. The stability of proposed algorithm is proved by Lyapunov approach. Besides, simulation results are given to demonstrate the effectiveness of proposed algorithm.

AB - This paper investigates the problem of multiple missiles attacking a fixed target coordinately. Different from the residual time cooperative control algorithm, direct relative distance control algorithm is designed in this paper. A finite-time simultaneous-arrival-to-origin (SATO) sliding mode control (SMC) algorithm for multi-missile systems (MMSs) is proposed. It is shown that the proposed algorithm can eliminate the singularity problem. Each missile under the algorithm can strike fixed targets simultaneously in finite-time. The stability of proposed algorithm is proved by Lyapunov approach. Besides, simulation results are given to demonstrate the effectiveness of proposed algorithm.

KW - Finite-time

KW - Multi-missile systems

KW - Simultaneous-arrival-to-origin

KW - Sliding model control

UR - http://www.scopus.com/inward/record.url?scp=85175551229&partnerID=8YFLogxK

U2 - 10.23919/CCC58697.2023.10240566

DO - 10.23919/CCC58697.2023.10240566

M3 - Conference contribution

AN - SCOPUS:85175551229

T3 - Chinese Control Conference, CCC

SP - 129

EP - 133

BT - 2023 42nd Chinese Control Conference, CCC 2023

PB - IEEE Computer Society

T2 - 42nd Chinese Control Conference, CCC 2023

Y2 - 24 July 2023 through 26 July 2023

ER -

Finite-time Simultaneous-Arrival-To-Origin Sliding Model Control for Multi-missile Systems

Abstract

Publication series

Conference

Keywords

Access to Document

Other files and links

Fingerprint

Cite this