Model Prediction Control for Missile Autopilot and Navigation

Tommy Pratama; Rusdhianto E.A. Kadir; Zulkifli Hidayat

doi:10.1109/CENIM48368.2019.8973362

Model Prediction Control for Missile Autopilot and Navigation

Tommy Pratama, Rusdhianto E.A. Kadir, Zulkifli Hidayat^*

^*Corresponding author for this work

Institut Teknologi Sepuluh Nopember

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

Abstract

Digital model predictive control (MPC) design for autopilot of missiles is presented in this paper. Missiles are systems that are nonlinear, Multi Input and Multi Output (MIMO), and coupled. As MPC is a control method for linear systems, the missile model needs to be linearized first by using the feedback linearization method. It is desired that the missile achieves its target by following a predefined path by governed by the nonlinear guidance logic. The effectiveness of the design is shown by a simulation of pursuing a moving target.

Original language	English
Title of host publication	2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 - Proceeding
Publisher	Institute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)	9781728129655
DOIs	https://doi.org/10.1109/CENIM48368.2019.8973362
Publication status	Published - Nov 2019
Externally published	Yes
Event	2nd International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 - Surabaya, Indonesia Duration: 19 Nov 2019 → 20 Nov 2019

Publication series

Name	2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 - Proceeding
Volume	2019-November

Conference

Conference	2nd International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019
Country/Territory	Indonesia
City	Surabaya
Period	19/11/19 → 20/11/19

Keywords

coupled system
discrete model
nonlinear feedback linearization
nonlinear guidance logic
predictive control
proportional navigation

Access to Document

10.1109/CENIM48368.2019.8973362

Cite this

Pratama, T., Kadir, R. E. A., & Hidayat, Z. (2019). Model Prediction Control for Missile Autopilot and Navigation. In 2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 - Proceeding Article 8973362 (2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 - Proceeding; Vol. 2019-November). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CENIM48368.2019.8973362

Pratama, Tommy ; Kadir, Rusdhianto E.A. ; Hidayat, Zulkifli. / Model Prediction Control for Missile Autopilot and Navigation. 2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 - Proceeding. Institute of Electrical and Electronics Engineers Inc., 2019. (2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 - Proceeding).

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title = "Model Prediction Control for Missile Autopilot and Navigation",

abstract = "Digital model predictive control (MPC) design for autopilot of missiles is presented in this paper. Missiles are systems that are nonlinear, Multi Input and Multi Output (MIMO), and coupled. As MPC is a control method for linear systems, the missile model needs to be linearized first by using the feedback linearization method. It is desired that the missile achieves its target by following a predefined path by governed by the nonlinear guidance logic. The effectiveness of the design is shown by a simulation of pursuing a moving target.",

keywords = "coupled system, discrete model, nonlinear feedback linearization, nonlinear guidance logic, predictive control, proportional navigation",

author = "Tommy Pratama and Kadir, {Rusdhianto E.A.} and Zulkifli Hidayat",

note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 2nd International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 ; Conference date: 19-11-2019 Through 20-11-2019",

year = "2019",

month = nov,

doi = "10.1109/CENIM48368.2019.8973362",

language = "English",

series = "2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 - Proceeding",

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

booktitle = "2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 - Proceeding",

address = "United States",

}

Pratama, T, Kadir, REA & Hidayat, Z 2019, Model Prediction Control for Missile Autopilot and Navigation. in 2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 - Proceeding., 8973362, 2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 - Proceeding, vol. 2019-November, Institute of Electrical and Electronics Engineers Inc., 2nd International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019, Surabaya, Indonesia, 19/11/19. https://doi.org/10.1109/CENIM48368.2019.8973362

Model Prediction Control for Missile Autopilot and Navigation. / Pratama, Tommy; Kadir, Rusdhianto E.A.; Hidayat, Zulkifli.
2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 - Proceeding. Institute of Electrical and Electronics Engineers Inc., 2019. 8973362 (2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 - Proceeding; Vol. 2019-November).

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

TY - GEN

T1 - Model Prediction Control for Missile Autopilot and Navigation

AU - Pratama, Tommy

AU - Kadir, Rusdhianto E.A.

AU - Hidayat, Zulkifli

PY - 2019/11

Y1 - 2019/11

N2 - Digital model predictive control (MPC) design for autopilot of missiles is presented in this paper. Missiles are systems that are nonlinear, Multi Input and Multi Output (MIMO), and coupled. As MPC is a control method for linear systems, the missile model needs to be linearized first by using the feedback linearization method. It is desired that the missile achieves its target by following a predefined path by governed by the nonlinear guidance logic. The effectiveness of the design is shown by a simulation of pursuing a moving target.

AB - Digital model predictive control (MPC) design for autopilot of missiles is presented in this paper. Missiles are systems that are nonlinear, Multi Input and Multi Output (MIMO), and coupled. As MPC is a control method for linear systems, the missile model needs to be linearized first by using the feedback linearization method. It is desired that the missile achieves its target by following a predefined path by governed by the nonlinear guidance logic. The effectiveness of the design is shown by a simulation of pursuing a moving target.

KW - coupled system

KW - discrete model

KW - nonlinear feedback linearization

KW - nonlinear guidance logic

KW - predictive control

KW - proportional navigation

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U2 - 10.1109/CENIM48368.2019.8973362

DO - 10.1109/CENIM48368.2019.8973362

M3 - Conference contribution

AN - SCOPUS:85084424984

T3 - 2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 - Proceeding

BT - 2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 - Proceeding

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2nd International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019

Y2 - 19 November 2019 through 20 November 2019

ER -

Pratama T, Kadir REA, Hidayat Z. Model Prediction Control for Missile Autopilot and Navigation. In 2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 - Proceeding. Institute of Electrical and Electronics Engineers Inc. 2019. 8973362. (2019 International Conference on Computer Engineering, Network, and Intelligent Multimedia, CENIM 2019 - Proceeding). doi: 10.1109/CENIM48368.2019.8973362

Model Prediction Control for Missile Autopilot and Navigation

Abstract

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Keywords

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