Firing logic design for ACS of missile with pulse jets

Yaxing Zhang; Baoqing Yang; Xin Huo; Songlin Chen

doi:10.1109/CCDC.2016.7531998

Firing logic design for ACS of missile with pulse jets

Yaxing Zhang
, Baoqing Yang
, Xin Huo
, Songlin Chen

School of Astronautics

Harbin Institute of Technology

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

3 Scopus citations

Abstract

In this paper, the problem of firing logic design is investigated for attitude control system (ACS) of air-defense missile with lateral jet control, aiming at improving the availability factor of the pulse jets. According to the features of pulse jets and some fire constraints, which are given in the form of mixed logic inequalities, an optimal quadratic performance index is proposed to minimize the jet force biases and total fired jets number. The optimization problem is solved by transforming the mixed-integer quadratic programming (MIQP) to mixed-integer linear programming(MILP), and the feasibility and practicability are illustrated by some numerical simulations in terminal guidance of missiles.

Original language	English
Title of host publication	Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	5596-5601
Number of pages	6
ISBN (Electronic)	9781467397148
DOIs	https://doi.org/10.1109/CCDC.2016.7531998
State	Published - 3 Aug 2016
Event	28th Chinese Control and Decision Conference, CCDC 2016 - Yinchuan, China Duration: 28 May 2016 → 30 May 2016

Publication series

Name	Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016

Conference

Conference	28th Chinese Control and Decision Conference, CCDC 2016
Country/Territory	China
City	Yinchuan
Period	28/05/16 → 30/05/16

Keywords

Attitude control system
MILP
Pulse jet

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10.1109/CCDC.2016.7531998

Cite this

Zhang, Y., Yang, B., Huo, X., & Chen, S. (2016). Firing logic design for ACS of missile with pulse jets. In Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016 (pp. 5596-5601). Article 7531998 (Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CCDC.2016.7531998

@inproceedings{edfb52f0a9644c498846c18e6d015270,

title = "Firing logic design for ACS of missile with pulse jets",

abstract = "In this paper, the problem of firing logic design is investigated for attitude control system (ACS) of air-defense missile with lateral jet control, aiming at improving the availability factor of the pulse jets. According to the features of pulse jets and some fire constraints, which are given in the form of mixed logic inequalities, an optimal quadratic performance index is proposed to minimize the jet force biases and total fired jets number. The optimization problem is solved by transforming the mixed-integer quadratic programming (MIQP) to mixed-integer linear programming(MILP), and the feasibility and practicability are illustrated by some numerical simulations in terminal guidance of missiles.",

keywords = "Attitude control system, MILP, Pulse jet",

author = "Yaxing Zhang and Baoqing Yang and Xin Huo and Songlin Chen",

note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; 28th Chinese Control and Decision Conference, CCDC 2016 ; Conference date: 28-05-2016 Through 30-05-2016",

year = "2016",

month = aug,

day = "3",

doi = "10.1109/CCDC.2016.7531998",

language = "英语",

series = "Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016",

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

pages = "5596--5601",

booktitle = "Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016",

address = "美国",

}

Zhang, Y, Yang, B , Huo, X & Chen, S 2016, Firing logic design for ACS of missile with pulse jets. in Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016., 7531998, Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016, Institute of Electrical and Electronics Engineers Inc., pp. 5596-5601, 28th Chinese Control and Decision Conference, CCDC 2016, Yinchuan, China, 28/05/16. https://doi.org/10.1109/CCDC.2016.7531998

Firing logic design for ACS of missile with pulse jets. / Zhang, Yaxing; Yang, Baoqing ; Huo, Xin et al.
Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016. Institute of Electrical and Electronics Engineers Inc., 2016. p. 5596-5601 7531998 (Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016).

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

TY - GEN

T1 - Firing logic design for ACS of missile with pulse jets

AU - Zhang, Yaxing

AU - Yang, Baoqing

AU - Huo, Xin

AU - Chen, Songlin

PY - 2016/8/3

Y1 - 2016/8/3

N2 - In this paper, the problem of firing logic design is investigated for attitude control system (ACS) of air-defense missile with lateral jet control, aiming at improving the availability factor of the pulse jets. According to the features of pulse jets and some fire constraints, which are given in the form of mixed logic inequalities, an optimal quadratic performance index is proposed to minimize the jet force biases and total fired jets number. The optimization problem is solved by transforming the mixed-integer quadratic programming (MIQP) to mixed-integer linear programming(MILP), and the feasibility and practicability are illustrated by some numerical simulations in terminal guidance of missiles.

AB - In this paper, the problem of firing logic design is investigated for attitude control system (ACS) of air-defense missile with lateral jet control, aiming at improving the availability factor of the pulse jets. According to the features of pulse jets and some fire constraints, which are given in the form of mixed logic inequalities, an optimal quadratic performance index is proposed to minimize the jet force biases and total fired jets number. The optimization problem is solved by transforming the mixed-integer quadratic programming (MIQP) to mixed-integer linear programming(MILP), and the feasibility and practicability are illustrated by some numerical simulations in terminal guidance of missiles.

KW - Attitude control system

KW - MILP

KW - Pulse jet

UR - https://www.scopus.com/pages/publications/84983760968

U2 - 10.1109/CCDC.2016.7531998

DO - 10.1109/CCDC.2016.7531998

M3 - 会议稿件

AN - SCOPUS:84983760968

T3 - Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016

SP - 5596

EP - 5601

BT - Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 28th Chinese Control and Decision Conference, CCDC 2016

Y2 - 28 May 2016 through 30 May 2016

ER -

Firing logic design for ACS of missile with pulse jets

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