Fixed-time guidance law for intercepting maneuvering targets with impact angle constraint

Xinxin Wang; Xianlin Huang; Shuchen Ding; Hongqian Lu

doi:10.23919/ChiCC.2019.8866644

Fixed-time guidance law for intercepting maneuvering targets with impact angle constraint

Xinxin Wang^*
, Xianlin Huang
, Shuchen Ding
, Hongqian Lu

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

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

2 Scopus citations

Abstract

Considering the problem of the missile for intercepting the maneuvering targets with the impact angle constraint, a novel adaptive fixed-time nonsingular fast terminal sliding mode guidance law (AFTNFTSMGL) is proposed in this paper. Firstly, a novel nonsingular fast terminal sliding mode (NFTSM) surface with fixed-time convergence regardless of the initial states is developed. Then, a modified AFTNFTSMGL is proposed based on the newly-defined NFTSM, where the unknown upper-bound of the unknown external disturbance caused by the target acceleration is estimated online by an adaptive law. The globally fixed-time stability of the proposed guidance law is derived with the Lyapunov methodology. Finally, simulation results show the effectiveness of the proposed guidance law.

Original language	English
Title of host publication	Proceedings of the 38th Chinese Control Conference, CCC 2019
Editors	Minyue Fu, Jian Sun
Publisher	IEEE Computer Society
Pages	3952-3957
Number of pages	6
ISBN (Electronic)	9789881563972
DOIs	https://doi.org/10.23919/ChiCC.2019.8866644
State	Published - Jul 2019
Event	38th Chinese Control Conference, CCC 2019 - Guangzhou, China Duration: 27 Jul 2019 → 30 Jul 2019

Publication series

Name	Chinese Control Conference, CCC
Volume	2019-July
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	38th Chinese Control Conference, CCC 2019
Country/Territory	China
City	Guangzhou
Period	27/07/19 → 30/07/19

Keywords

Fixed-time convergence
Guidance law
Impact angle constraint
Nonsingular fast terminal sliding mode

Access to Document

10.23919/ChiCC.2019.8866644

Cite this

Wang, X., Huang, X., Ding, S., & Lu, H. (2019). Fixed-time guidance law for intercepting maneuvering targets with impact angle constraint. In M. Fu, & J. Sun (Eds.), Proceedings of the 38th Chinese Control Conference, CCC 2019 (pp. 3952-3957). Article 8866644 (Chinese Control Conference, CCC; Vol. 2019-July). IEEE Computer Society. https://doi.org/10.23919/ChiCC.2019.8866644

@inproceedings{c45931aa5ded4daeb6162d0f5c7f6b07,

title = "Fixed-time guidance law for intercepting maneuvering targets with impact angle constraint",

abstract = "Considering the problem of the missile for intercepting the maneuvering targets with the impact angle constraint, a novel adaptive fixed-time nonsingular fast terminal sliding mode guidance law (AFTNFTSMGL) is proposed in this paper. Firstly, a novel nonsingular fast terminal sliding mode (NFTSM) surface with fixed-time convergence regardless of the initial states is developed. Then, a modified AFTNFTSMGL is proposed based on the newly-defined NFTSM, where the unknown upper-bound of the unknown external disturbance caused by the target acceleration is estimated online by an adaptive law. The globally fixed-time stability of the proposed guidance law is derived with the Lyapunov methodology. Finally, simulation results show the effectiveness of the proposed guidance law.",

keywords = "Fixed-time convergence, Guidance law, Impact angle constraint, Nonsingular fast terminal sliding mode",

author = "Xinxin Wang and Xianlin Huang and Shuchen Ding and Hongqian Lu",

note = "Publisher Copyright: {\textcopyright} 2019 Technical Committee on Control Theory, Chinese Association of Automation.; 38th Chinese Control Conference, CCC 2019 ; Conference date: 27-07-2019 Through 30-07-2019",

year = "2019",

month = jul,

doi = "10.23919/ChiCC.2019.8866644",

language = "英语",

series = "Chinese Control Conference, CCC",

publisher = "IEEE Computer Society",

pages = "3952--3957",

editor = "Minyue Fu and Jian Sun",

booktitle = "Proceedings of the 38th Chinese Control Conference, CCC 2019",

address = "美国",

}

Wang, X, Huang, X, Ding, S & Lu, H 2019, Fixed-time guidance law for intercepting maneuvering targets with impact angle constraint. in M Fu & J Sun (eds), Proceedings of the 38th Chinese Control Conference, CCC 2019., 8866644, Chinese Control Conference, CCC, vol. 2019-July, IEEE Computer Society, pp. 3952-3957, 38th Chinese Control Conference, CCC 2019, Guangzhou, China, 27/07/19. https://doi.org/10.23919/ChiCC.2019.8866644

Fixed-time guidance law for intercepting maneuvering targets with impact angle constraint. / Wang, Xinxin; Huang, Xianlin; Ding, Shuchen et al.
Proceedings of the 38th Chinese Control Conference, CCC 2019. ed. / Minyue Fu; Jian Sun. IEEE Computer Society, 2019. p. 3952-3957 8866644 (Chinese Control Conference, CCC; Vol. 2019-July).

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

TY - GEN

T1 - Fixed-time guidance law for intercepting maneuvering targets with impact angle constraint

AU - Wang, Xinxin

AU - Huang, Xianlin

AU - Ding, Shuchen

AU - Lu, Hongqian

PY - 2019/7

Y1 - 2019/7

N2 - Considering the problem of the missile for intercepting the maneuvering targets with the impact angle constraint, a novel adaptive fixed-time nonsingular fast terminal sliding mode guidance law (AFTNFTSMGL) is proposed in this paper. Firstly, a novel nonsingular fast terminal sliding mode (NFTSM) surface with fixed-time convergence regardless of the initial states is developed. Then, a modified AFTNFTSMGL is proposed based on the newly-defined NFTSM, where the unknown upper-bound of the unknown external disturbance caused by the target acceleration is estimated online by an adaptive law. The globally fixed-time stability of the proposed guidance law is derived with the Lyapunov methodology. Finally, simulation results show the effectiveness of the proposed guidance law.

AB - Considering the problem of the missile for intercepting the maneuvering targets with the impact angle constraint, a novel adaptive fixed-time nonsingular fast terminal sliding mode guidance law (AFTNFTSMGL) is proposed in this paper. Firstly, a novel nonsingular fast terminal sliding mode (NFTSM) surface with fixed-time convergence regardless of the initial states is developed. Then, a modified AFTNFTSMGL is proposed based on the newly-defined NFTSM, where the unknown upper-bound of the unknown external disturbance caused by the target acceleration is estimated online by an adaptive law. The globally fixed-time stability of the proposed guidance law is derived with the Lyapunov methodology. Finally, simulation results show the effectiveness of the proposed guidance law.

KW - Fixed-time convergence

KW - Guidance law

KW - Impact angle constraint

KW - Nonsingular fast terminal sliding mode

UR - https://www.scopus.com/pages/publications/85074398577

U2 - 10.23919/ChiCC.2019.8866644

DO - 10.23919/ChiCC.2019.8866644

M3 - 会议稿件

AN - SCOPUS:85074398577

T3 - Chinese Control Conference, CCC

SP - 3952

EP - 3957

BT - Proceedings of the 38th Chinese Control Conference, CCC 2019

A2 - Fu, Minyue

A2 - Sun, Jian

PB - IEEE Computer Society

T2 - 38th Chinese Control Conference, CCC 2019

Y2 - 27 July 2019 through 30 July 2019

ER -

Fixed-time guidance law for intercepting maneuvering targets with impact angle constraint

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