Fractional calculus guidance algorithm for aircraft pursuit-evasion

Jian Chen; Shubo Wang; Wei Wang; Yu Tan; Yongjun Zheng; Zhang Ren

doi:10.1109/CCDC.2017.7978612

Fractional calculus guidance algorithm for aircraft pursuit-evasion

Jian Chen
, Shubo Wang
, Wei Wang
, Yu Tan
, Yongjun Zheng
, Zhang Ren

School of Automation Science and Electrical Engineering

China Agricultural University
Hunan University of Finance and Economics

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

Abstract

Aiming at intercepting hypersonic target in a pursuit-evasion game, this paper presents a fractional calculus guidance algorithm based on a Nonlinear Proportional and Differential Guidance law (NPDG). According to relative motions between the interceptor and target, quantitative values were proposed for the parameters of the fractional calculus guidance law and system stability condition was given. Numerical experiment results demonstrated that the proposed guidance algorithm effectively reduced the miss distance against target maneuver. A stronger robustness compared to the NPDG was also shown under noisy condition.

Original language	English
Title of host publication	Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	7817-7821
Number of pages	5
ISBN (Electronic)	9781509046560
DOIs	https://doi.org/10.1109/CCDC.2017.7978612
State	Published - 12 Jul 2017
Event	29th Chinese Control and Decision Conference, CCDC 2017 - Chongqing, China Duration: 28 May 2017 → 30 May 2017

Publication series

Name	Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017

Conference

Conference	29th Chinese Control and Decision Conference, CCDC 2017
Country/Territory	China
City	Chongqing
Period	28/05/17 → 30/05/17

Keywords

Fractional Calculus
Guidance Law
Pursuit-evasion Game
Target Maneuver

Access to Document

10.1109/CCDC.2017.7978612

Cite this

Chen, J., Wang, S., Wang, W., Tan, Y., Zheng, Y., & Ren, Z. (2017). Fractional calculus guidance algorithm for aircraft pursuit-evasion. In Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017 (pp. 7817-7821). Article 7978612 (Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CCDC.2017.7978612

@inproceedings{ac88a480a13849d6a935c7a52c96bdb5,

title = "Fractional calculus guidance algorithm for aircraft pursuit-evasion",

abstract = "Aiming at intercepting hypersonic target in a pursuit-evasion game, this paper presents a fractional calculus guidance algorithm based on a Nonlinear Proportional and Differential Guidance law (NPDG). According to relative motions between the interceptor and target, quantitative values were proposed for the parameters of the fractional calculus guidance law and system stability condition was given. Numerical experiment results demonstrated that the proposed guidance algorithm effectively reduced the miss distance against target maneuver. A stronger robustness compared to the NPDG was also shown under noisy condition.",

keywords = "Fractional Calculus, Guidance Law, Pursuit-evasion Game, Target Maneuver",

author = "Jian Chen and Shubo Wang and Wei Wang and Yu Tan and Yongjun Zheng and Zhang Ren",

note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 29th Chinese Control and Decision Conference, CCDC 2017 ; Conference date: 28-05-2017 Through 30-05-2017",

year = "2017",

month = jul,

day = "12",

doi = "10.1109/CCDC.2017.7978612",

language = "英语",

series = "Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017",

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

pages = "7817--7821",

booktitle = "Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017",

address = "美国",

}

Chen, J, Wang, S, Wang, W, Tan, Y, Zheng, Y & Ren, Z 2017, Fractional calculus guidance algorithm for aircraft pursuit-evasion. in Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017., 7978612, Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017, Institute of Electrical and Electronics Engineers Inc., pp. 7817-7821, 29th Chinese Control and Decision Conference, CCDC 2017, Chongqing, China, 28/05/17. https://doi.org/10.1109/CCDC.2017.7978612

Fractional calculus guidance algorithm for aircraft pursuit-evasion. / Chen, Jian; Wang, Shubo; Wang, Wei et al.
Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017. Institute of Electrical and Electronics Engineers Inc., 2017. p. 7817-7821 7978612 (Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017).

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

TY - GEN

T1 - Fractional calculus guidance algorithm for aircraft pursuit-evasion

AU - Chen, Jian

AU - Wang, Shubo

AU - Wang, Wei

AU - Tan, Yu

AU - Zheng, Yongjun

AU - Ren, Zhang

PY - 2017/7/12

Y1 - 2017/7/12

N2 - Aiming at intercepting hypersonic target in a pursuit-evasion game, this paper presents a fractional calculus guidance algorithm based on a Nonlinear Proportional and Differential Guidance law (NPDG). According to relative motions between the interceptor and target, quantitative values were proposed for the parameters of the fractional calculus guidance law and system stability condition was given. Numerical experiment results demonstrated that the proposed guidance algorithm effectively reduced the miss distance against target maneuver. A stronger robustness compared to the NPDG was also shown under noisy condition.

AB - Aiming at intercepting hypersonic target in a pursuit-evasion game, this paper presents a fractional calculus guidance algorithm based on a Nonlinear Proportional and Differential Guidance law (NPDG). According to relative motions between the interceptor and target, quantitative values were proposed for the parameters of the fractional calculus guidance law and system stability condition was given. Numerical experiment results demonstrated that the proposed guidance algorithm effectively reduced the miss distance against target maneuver. A stronger robustness compared to the NPDG was also shown under noisy condition.

KW - Fractional Calculus

KW - Guidance Law

KW - Pursuit-evasion Game

KW - Target Maneuver

UR - https://www.scopus.com/pages/publications/85028086213

U2 - 10.1109/CCDC.2017.7978612

DO - 10.1109/CCDC.2017.7978612

M3 - 会议稿件

AN - SCOPUS:85028086213

T3 - Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017

SP - 7817

EP - 7821

BT - Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 29th Chinese Control and Decision Conference, CCDC 2017

Y2 - 28 May 2017 through 30 May 2017

ER -

Chen J, Wang S, Wang W, Tan Y, Zheng Y, Ren Z. Fractional calculus guidance algorithm for aircraft pursuit-evasion. In Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017. Institute of Electrical and Electronics Engineers Inc. 2017. p. 7817-7821. 7978612. (Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017). doi: 10.1109/CCDC.2017.7978612

Fractional calculus guidance algorithm for aircraft pursuit-evasion

Abstract

Publication series

Conference

Keywords

Access to Document

Other files and links

Fingerprint

Cite this