Autopilot design for a side-jet missile based on MRVSS with an adaptive approach law

Jian Chen; Hugh H.T. Liu; Zhang Ren

Autopilot design for a side-jet missile based on MRVSS with an adaptive approach law

Jian Chen^*
, Hugh H.T. Liu
, Zhang Ren

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Beihang University
University of Toronto

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

2 Scopus citations

Abstract

The autopilot design of a side jet and aero-fin blending control air-to-air missile is discussed in this paper and a Model Reference Variable Sliding Structure (MRVSS) method is presented. The side jets are in the discontinuous on-off pulse forms which are different from the conventional continuous side jets. The control parameters are sought though Genetic Algorithm (GA). Further, a novel adaptive variable-rate exponential approach law is introduced to approach the sliding surface quickly. The proposed method is verified by simulations on a research side-jet missile model and it's convenient to be carried out on other multi-actuator applications which is meaningful in actual engineering.

Original language	English
Title of host publication	Proceedings of the 29th Chinese Control Conference, CCC'10
Pages	2293-2298
Number of pages	6
State	Published - 2010
Event	29th Chinese Control Conference, CCC'10 - Beijing, China Duration: 29 Jul 2010 → 31 Jul 2010

Publication series

Name	Proceedings of the 29th Chinese Control Conference, CCC'10

Conference

Conference	29th Chinese Control Conference, CCC'10
Country/Territory	China
City	Beijing
Period	29/07/10 → 31/07/10

Keywords

Adaptive approach law
Model Reference Variable Sliding Structure
Side jet

Cite this

@inproceedings{c65a261549b643859748ca948b015941,

title = "Autopilot design for a side-jet missile based on MRVSS with an adaptive approach law",

abstract = "The autopilot design of a side jet and aero-fin blending control air-to-air missile is discussed in this paper and a Model Reference Variable Sliding Structure (MRVSS) method is presented. The side jets are in the discontinuous on-off pulse forms which are different from the conventional continuous side jets. The control parameters are sought though Genetic Algorithm (GA). Further, a novel adaptive variable-rate exponential approach law is introduced to approach the sliding surface quickly. The proposed method is verified by simulations on a research side-jet missile model and it's convenient to be carried out on other multi-actuator applications which is meaningful in actual engineering.",

keywords = "Adaptive approach law, Model Reference Variable Sliding Structure, Side jet",

author = "Jian Chen and Liu, \{Hugh H.T.\} and Zhang Ren",

year = "2010",

language = "英语",

isbn = "9787894631046",

series = "Proceedings of the 29th Chinese Control Conference, CCC'10",

pages = "2293--2298",

booktitle = "Proceedings of the 29th Chinese Control Conference, CCC'10",

note = "29th Chinese Control Conference, CCC'10 ; Conference date: 29-07-2010 Through 31-07-2010",

}

Autopilot design for a side-jet missile based on MRVSS with an adaptive approach law. / Chen, Jian; Liu, Hugh H.T.; Ren, Zhang.
Proceedings of the 29th Chinese Control Conference, CCC'10. 2010. p. 2293-2298 5573273 (Proceedings of the 29th Chinese Control Conference, CCC'10).

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

TY - GEN

T1 - Autopilot design for a side-jet missile based on MRVSS with an adaptive approach law

AU - Chen, Jian

AU - Liu, Hugh H.T.

AU - Ren, Zhang

PY - 2010

Y1 - 2010

N2 - The autopilot design of a side jet and aero-fin blending control air-to-air missile is discussed in this paper and a Model Reference Variable Sliding Structure (MRVSS) method is presented. The side jets are in the discontinuous on-off pulse forms which are different from the conventional continuous side jets. The control parameters are sought though Genetic Algorithm (GA). Further, a novel adaptive variable-rate exponential approach law is introduced to approach the sliding surface quickly. The proposed method is verified by simulations on a research side-jet missile model and it's convenient to be carried out on other multi-actuator applications which is meaningful in actual engineering.

AB - The autopilot design of a side jet and aero-fin blending control air-to-air missile is discussed in this paper and a Model Reference Variable Sliding Structure (MRVSS) method is presented. The side jets are in the discontinuous on-off pulse forms which are different from the conventional continuous side jets. The control parameters are sought though Genetic Algorithm (GA). Further, a novel adaptive variable-rate exponential approach law is introduced to approach the sliding surface quickly. The proposed method is verified by simulations on a research side-jet missile model and it's convenient to be carried out on other multi-actuator applications which is meaningful in actual engineering.

KW - Adaptive approach law

KW - Model Reference Variable Sliding Structure

KW - Side jet

UR - https://www.scopus.com/pages/publications/78650247174

M3 - 会议稿件

AN - SCOPUS:78650247174

SN - 9787894631046

T3 - Proceedings of the 29th Chinese Control Conference, CCC'10

SP - 2293

EP - 2298

BT - Proceedings of the 29th Chinese Control Conference, CCC'10

T2 - 29th Chinese Control Conference, CCC'10

Y2 - 29 July 2010 through 31 July 2010

ER -

Autopilot design for a side-jet missile based on MRVSS with an adaptive approach law

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Keywords

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