Model predictive control for a missile with blended lateral jets and aerodynamic fins

Fenghua He; Kemao Ma; Baoqing Yang; Yu Yao

doi:10.1109/CHICC.2008.4605718

Model predictive control for a missile with blended lateral jets and aerodynamic fins

Fenghua He^*
, Kemao Ma
, Baoqing Yang
, Yu Yao

^*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

For a missile with blended lateral jets and aerodynamic fins, the problem of output tracking, that is the tracking of lateral acceleration of missile, is discussed in this paper. Since the fast response requirement on the lateral acceleration, lateral jets are preferable to aerodynamic fins, both of which can provide attitude control torque, but with different response speeds. For this situation, the output is described via Fliess functional expansion based on the discrete characteristic of lateral jets. The design for control law of lateral jets attitude control system is formulated to an optimization problem. Simulation results show the effectiveness of the proposed method.

Original language	English
Title of host publication	Proceedings of the 27th Chinese Control Conference, CCC
Pages	430-434
Number of pages	5
DOIs	https://doi.org/10.1109/CHICC.2008.4605718
State	Published - 2008
Event	27th Chinese Control Conference, CCC - Kunming, Yunnan, China Duration: 16 Jul 2008 → 18 Jul 2008

Publication series

Name	Proceedings of the 27th Chinese Control Conference, CCC

Conference

Conference	27th Chinese Control Conference, CCC
Country/Territory	China
City	Kunming, Yunnan
Period	16/07/08 → 18/07/08

Keywords

Fliess functional expansion
Lateral jets
Missile
Output predictive control
Output tracking

Access to Document

10.1109/CHICC.2008.4605718

Cite this

@inproceedings{f8a280253c9a4741a90625818dbc0d2f,

title = "Model predictive control for a missile with blended lateral jets and aerodynamic fins",

abstract = "For a missile with blended lateral jets and aerodynamic fins, the problem of output tracking, that is the tracking of lateral acceleration of missile, is discussed in this paper. Since the fast response requirement on the lateral acceleration, lateral jets are preferable to aerodynamic fins, both of which can provide attitude control torque, but with different response speeds. For this situation, the output is described via Fliess functional expansion based on the discrete characteristic of lateral jets. The design for control law of lateral jets attitude control system is formulated to an optimization problem. Simulation results show the effectiveness of the proposed method.",

keywords = "Fliess functional expansion, Lateral jets, Missile, Output predictive control, Output tracking",

author = "Fenghua He and Kemao Ma and Baoqing Yang and Yu Yao",

year = "2008",

doi = "10.1109/CHICC.2008.4605718",

language = "英语",

isbn = "9787900719706",

series = "Proceedings of the 27th Chinese Control Conference, CCC",

pages = "430--434",

booktitle = "Proceedings of the 27th Chinese Control Conference, CCC",

note = "27th Chinese Control Conference, CCC ; Conference date: 16-07-2008 Through 18-07-2008",

}

He, F , Ma, K , Yang, B & Yao, Y 2008, Model predictive control for a missile with blended lateral jets and aerodynamic fins. in Proceedings of the 27th Chinese Control Conference, CCC., 4605718, Proceedings of the 27th Chinese Control Conference, CCC, pp. 430-434, 27th Chinese Control Conference, CCC, Kunming, Yunnan, China, 16/07/08. https://doi.org/10.1109/CHICC.2008.4605718

Model predictive control for a missile with blended lateral jets and aerodynamic fins. / He, Fenghua ; Ma, Kemao ; Yang, Baoqing et al.
Proceedings of the 27th Chinese Control Conference, CCC. 2008. p. 430-434 4605718 (Proceedings of the 27th Chinese Control Conference, CCC).

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

TY - GEN

T1 - Model predictive control for a missile with blended lateral jets and aerodynamic fins

AU - He, Fenghua

AU - Ma, Kemao

AU - Yang, Baoqing

AU - Yao, Yu

PY - 2008

Y1 - 2008

N2 - For a missile with blended lateral jets and aerodynamic fins, the problem of output tracking, that is the tracking of lateral acceleration of missile, is discussed in this paper. Since the fast response requirement on the lateral acceleration, lateral jets are preferable to aerodynamic fins, both of which can provide attitude control torque, but with different response speeds. For this situation, the output is described via Fliess functional expansion based on the discrete characteristic of lateral jets. The design for control law of lateral jets attitude control system is formulated to an optimization problem. Simulation results show the effectiveness of the proposed method.

AB - For a missile with blended lateral jets and aerodynamic fins, the problem of output tracking, that is the tracking of lateral acceleration of missile, is discussed in this paper. Since the fast response requirement on the lateral acceleration, lateral jets are preferable to aerodynamic fins, both of which can provide attitude control torque, but with different response speeds. For this situation, the output is described via Fliess functional expansion based on the discrete characteristic of lateral jets. The design for control law of lateral jets attitude control system is formulated to an optimization problem. Simulation results show the effectiveness of the proposed method.

KW - Fliess functional expansion

KW - Lateral jets

KW - Missile

KW - Output predictive control

KW - Output tracking

UR - https://www.scopus.com/pages/publications/52449093418

U2 - 10.1109/CHICC.2008.4605718

DO - 10.1109/CHICC.2008.4605718

M3 - 会议稿件

AN - SCOPUS:52449093418

SN - 9787900719706

T3 - Proceedings of the 27th Chinese Control Conference, CCC

SP - 430

EP - 434

BT - Proceedings of the 27th Chinese Control Conference, CCC

T2 - 27th Chinese Control Conference, CCC

Y2 - 16 July 2008 through 18 July 2008

ER -

Model predictive control for a missile with blended lateral jets and aerodynamic fins

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Publication series

Conference

Keywords

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