Research on the new missile actuation system with dual independent closed-loop

Hui Chen; Yong Ling Fu; Juan Chen; He Song Liu

doi:10.4028/www.scientific.net/AMM.551.337

Research on the new missile actuation system with dual independent closed-loop

Hui Chen^*
, Yong Ling Fu
, Juan Chen
, He Song Liu

^*Corresponding author for this work

School of Mechanical Engineering and Automation

Beihang University

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

Abstract

With the development of the advanced precision-guided missile and anti-missile system, high precision, high penetration ability and Low energy consumption have become an important direction for the missile. A new missile electro-hydraulic actuation system with dual independent closed-loop is put forward with the trend of high performance and energy-saving, and then the operating principle and process are discussed. Finally the accurate mathematical model is established, and the influence of the different basic pressure on the dynamic performance is analyzed. The simulation results show that the new proposed scheme has made great improvements in reducing the zero-control current of the system, but the efficiency and performance of the actuation system should be considered integrated due to the decrease of the dynamic performance, so it is practical for the future development of the missile electro-hydraulic actuation system.

Original language	English
Title of host publication	Design, Manufacturing and Mechatronics
Publisher	Trans Tech Publications
Pages	337-343
Number of pages	7
ISBN (Print)	9783038351016
DOIs	https://doi.org/10.4028/www.scientific.net/AMM.551.337
State	Published - 2014
Event	2014 International Conference on Design, Manufacturing and Mechatronics, ICDMM 2014 - Changsha, Hunan, China Duration: 21 Mar 2014 → 23 Mar 2014

Publication series

Name	Applied Mechanics and Materials
Volume	551
ISSN (Print)	1660-9336
ISSN (Electronic)	1662-7482

Conference

Conference	2014 International Conference on Design, Manufacturing and Mechatronics, ICDMM 2014
Country/Territory	China
City	Changsha, Hunan
Period	21/03/14 → 23/03/14

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

SDG 7 Affordable and Clean Energy

Keywords

Electro-hydraulic actuator
Missile
Pressure control

Access to Document

10.4028/www.scientific.net/AMM.551.337

Cite this

@inproceedings{892764be6d6e4515b25365431fce6a91,

title = "Research on the new missile actuation system with dual independent closed-loop",

abstract = "With the development of the advanced precision-guided missile and anti-missile system, high precision, high penetration ability and Low energy consumption have become an important direction for the missile. A new missile electro-hydraulic actuation system with dual independent closed-loop is put forward with the trend of high performance and energy-saving, and then the operating principle and process are discussed. Finally the accurate mathematical model is established, and the influence of the different basic pressure on the dynamic performance is analyzed. The simulation results show that the new proposed scheme has made great improvements in reducing the zero-control current of the system, but the efficiency and performance of the actuation system should be considered integrated due to the decrease of the dynamic performance, so it is practical for the future development of the missile electro-hydraulic actuation system.",

keywords = "Electro-hydraulic actuator, Missile, Pressure control",

author = "Hui Chen and Fu, \{Yong Ling\} and Juan Chen and Liu, \{He Song\}",

year = "2014",

doi = "10.4028/www.scientific.net/AMM.551.337",

language = "英语",

isbn = "9783038351016",

series = "Applied Mechanics and Materials",

publisher = "Trans Tech Publications",

pages = "337--343",

booktitle = "Design, Manufacturing and Mechatronics",

address = "德国",

note = "2014 International Conference on Design, Manufacturing and Mechatronics, ICDMM 2014 ; Conference date: 21-03-2014 Through 23-03-2014",

}

Chen, H, Fu, YL , Chen, J & Liu, HS 2014, Research on the new missile actuation system with dual independent closed-loop. in Design, Manufacturing and Mechatronics. Applied Mechanics and Materials, vol. 551, Trans Tech Publications, pp. 337-343, 2014 International Conference on Design, Manufacturing and Mechatronics, ICDMM 2014, Changsha, Hunan, China, 21/03/14. https://doi.org/10.4028/www.scientific.net/AMM.551.337

TY - GEN

T1 - Research on the new missile actuation system with dual independent closed-loop

AU - Chen, Hui

AU - Fu, Yong Ling

AU - Chen, Juan

AU - Liu, He Song

PY - 2014

Y1 - 2014

N2 - With the development of the advanced precision-guided missile and anti-missile system, high precision, high penetration ability and Low energy consumption have become an important direction for the missile. A new missile electro-hydraulic actuation system with dual independent closed-loop is put forward with the trend of high performance and energy-saving, and then the operating principle and process are discussed. Finally the accurate mathematical model is established, and the influence of the different basic pressure on the dynamic performance is analyzed. The simulation results show that the new proposed scheme has made great improvements in reducing the zero-control current of the system, but the efficiency and performance of the actuation system should be considered integrated due to the decrease of the dynamic performance, so it is practical for the future development of the missile electro-hydraulic actuation system.

AB - With the development of the advanced precision-guided missile and anti-missile system, high precision, high penetration ability and Low energy consumption have become an important direction for the missile. A new missile electro-hydraulic actuation system with dual independent closed-loop is put forward with the trend of high performance and energy-saving, and then the operating principle and process are discussed. Finally the accurate mathematical model is established, and the influence of the different basic pressure on the dynamic performance is analyzed. The simulation results show that the new proposed scheme has made great improvements in reducing the zero-control current of the system, but the efficiency and performance of the actuation system should be considered integrated due to the decrease of the dynamic performance, so it is practical for the future development of the missile electro-hydraulic actuation system.

KW - Electro-hydraulic actuator

KW - Missile

KW - Pressure control

UR - https://www.scopus.com/pages/publications/84901441463

U2 - 10.4028/www.scientific.net/AMM.551.337

DO - 10.4028/www.scientific.net/AMM.551.337

M3 - 会议稿件

AN - SCOPUS:84901441463

SN - 9783038351016

T3 - Applied Mechanics and Materials

SP - 337

EP - 343

BT - Design, Manufacturing and Mechatronics

PB - Trans Tech Publications

T2 - 2014 International Conference on Design, Manufacturing and Mechatronics, ICDMM 2014

Y2 - 21 March 2014 through 23 March 2014

ER -

Research on the new missile actuation system with dual independent closed-loop

Abstract

Publication series

Conference

UN SDGs

Keywords

Access to Document

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