Missile autopilot design using backstepping approach

De Fu Lin; Jun Fang Fan

doi:10.1109/ICCEE.2009.51

Missile autopilot design using backstepping approach

De Fu Lin^*, Jun Fang Fan

^*Corresponding author for this work

School of Aerospace Engineering

Beijing Information Science & Technology University

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

4 Citations (Scopus)

Abstract

The autopilot design process is detailed from a backstepping control perspective. The control parameters were determined based on step and sine input commands. Then both characteristics and effect of two control parameters were examined. A linear three-loop topology was also presented for comparison. The results show that the backstepping recursive approach provides a systematically constructive procedure for acceleration autopilot. The based nonlinear autopilot exhibits excellent tracking and robustness.

Original language	English
Title of host publication	2009 International Conference on Computer and Electrical Engineering, ICCEE 2009
Pages	238-241
Number of pages	4
DOIs	https://doi.org/10.1109/ICCEE.2009.51
Publication status	Published - 2009
Event	2009 International Conference on Computer and Electrical Engineering, ICCEE 2009 - Dubai, United Arab Emirates Duration: 28 Dec 2009 → 30 Dec 2009

Publication series

Name	2009 International Conference on Computer and Electrical Engineering, ICCEE 2009
Volume	1

Conference

Conference	2009 International Conference on Computer and Electrical Engineering, ICCEE 2009
Country/Territory	United Arab Emirates
City	Dubai
Period	28/12/09 → 30/12/09

Keywords

Acceleration autopilot
Backstepping
Missile control
Optimal control

Access to Document

10.1109/ICCEE.2009.51

Cite this

@inproceedings{190ca8f69b5744f189b054d2bb3df546,

title = "Missile autopilot design using backstepping approach",

abstract = "The autopilot design process is detailed from a backstepping control perspective. The control parameters were determined based on step and sine input commands. Then both characteristics and effect of two control parameters were examined. A linear three-loop topology was also presented for comparison. The results show that the backstepping recursive approach provides a systematically constructive procedure for acceleration autopilot. The based nonlinear autopilot exhibits excellent tracking and robustness.",

keywords = "Acceleration autopilot, Backstepping, Missile control, Optimal control",

author = "Lin, {De Fu} and Fan, {Jun Fang}",

year = "2009",

doi = "10.1109/ICCEE.2009.51",

language = "English",

isbn = "9780769539256",

series = "2009 International Conference on Computer and Electrical Engineering, ICCEE 2009",

pages = "238--241",

booktitle = "2009 International Conference on Computer and Electrical Engineering, ICCEE 2009",

note = "2009 International Conference on Computer and Electrical Engineering, ICCEE 2009 ; Conference date: 28-12-2009 Through 30-12-2009",

}

Lin, DF & Fan, JF 2009, Missile autopilot design using backstepping approach. in 2009 International Conference on Computer and Electrical Engineering, ICCEE 2009., 5380494, 2009 International Conference on Computer and Electrical Engineering, ICCEE 2009, vol. 1, pp. 238-241, 2009 International Conference on Computer and Electrical Engineering, ICCEE 2009, Dubai, United Arab Emirates, 28/12/09. https://doi.org/10.1109/ICCEE.2009.51

Missile autopilot design using backstepping approach. / Lin, De Fu; Fan, Jun Fang.
2009 International Conference on Computer and Electrical Engineering, ICCEE 2009. 2009. p. 238-241 5380494 (2009 International Conference on Computer and Electrical Engineering, ICCEE 2009; Vol. 1).

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

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AB - The autopilot design process is detailed from a backstepping control perspective. The control parameters were determined based on step and sine input commands. Then both characteristics and effect of two control parameters were examined. A linear three-loop topology was also presented for comparison. The results show that the backstepping recursive approach provides a systematically constructive procedure for acceleration autopilot. The based nonlinear autopilot exhibits excellent tracking and robustness.

KW - Acceleration autopilot

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KW - Missile control

KW - Optimal control

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Y2 - 28 December 2009 through 30 December 2009

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Missile autopilot design using backstepping approach

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Keywords

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