Research on inverse system decoupling of three-axis flight simulator based on the high-speed rotation missile

Xin Ying Yan; Bo Mo; Yang Hua Li

doi:10.4028/www.scientific.net/AMM.615.323

Research on inverse system decoupling of three-axis flight simulator based on the high-speed rotation missile

Xin Ying Yan, Bo Mo, Yang Hua Li

School of Aerospace Engineering

Beijing Institute of Technology

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

Abstract

This paper researches on the kinematics and dynamics of coupling for three-axis flight Simulator based on the high-speed rotation missile. Firstly, to define station body coordinate and the positive direction of rotation according to three-axis flight Simulator based on the high-speed rotation missile, and then the mathematical coupling model is established. Secondly, multivariable nonlinear mathematical model can be decoupling, while substituting the parameters quality attribute analysis solved by ProE into the mathematical model. Lastly, the decoupled linear equations and the decoupling solutions based on inverse system method were given, and then to finish the simulation and to analysis the simulation results.

Original language	English
Title of host publication	Automatic Control and Mechatronic Engineering III
Publisher	Trans Tech Publications Ltd.
Pages	323-328
Number of pages	6
ISBN (Print)	9783038351993
DOIs	https://doi.org/10.4028/www.scientific.net/AMM.615.323
Publication status	Published - 2014
Event	3rd International Conference on Automatic Control and Mechatronic Engineering, ICACME 2014 - Xiamen, China Duration: 13 Jun 2014 → 14 Jun 2014

Publication series

Name	Applied Mechanics and Materials
Volume	615
ISSN (Print)	1660-9336
ISSN (Electronic)	1662-7482

Conference

Conference	3rd International Conference on Automatic Control and Mechatronic Engineering, ICACME 2014
Country/Territory	China
City	Xiamen
Period	13/06/14 → 14/06/14

Keywords

Decoupling
High-speed rotation missile
Inverse system
Three-axis flight simulator

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10.4028/www.scientific.net/AMM.615.323

Cite this

@inproceedings{de0410474cbd44618011e98e1ec0502e,

title = "Research on inverse system decoupling of three-axis flight simulator based on the high-speed rotation missile",

abstract = "This paper researches on the kinematics and dynamics of coupling for three-axis flight Simulator based on the high-speed rotation missile. Firstly, to define station body coordinate and the positive direction of rotation according to three-axis flight Simulator based on the high-speed rotation missile, and then the mathematical coupling model is established. Secondly, multivariable nonlinear mathematical model can be decoupling, while substituting the parameters quality attribute analysis solved by ProE into the mathematical model. Lastly, the decoupled linear equations and the decoupling solutions based on inverse system method were given, and then to finish the simulation and to analysis the simulation results.",

keywords = "Decoupling, High-speed rotation missile, Inverse system, Three-axis flight simulator",

author = "Yan, {Xin Ying} and Bo Mo and Li, {Yang Hua}",

year = "2014",

doi = "10.4028/www.scientific.net/AMM.615.323",

language = "English",

isbn = "9783038351993",

series = "Applied Mechanics and Materials",

publisher = "Trans Tech Publications Ltd.",

pages = "323--328",

booktitle = "Automatic Control and Mechatronic Engineering III",

address = "Switzerland",

note = "3rd International Conference on Automatic Control and Mechatronic Engineering, ICACME 2014 ; Conference date: 13-06-2014 Through 14-06-2014",

}

Yan, XY, Mo, B & Li, YH 2014, Research on inverse system decoupling of three-axis flight simulator based on the high-speed rotation missile. in Automatic Control and Mechatronic Engineering III. Applied Mechanics and Materials, vol. 615, Trans Tech Publications Ltd., pp. 323-328, 3rd International Conference on Automatic Control and Mechatronic Engineering, ICACME 2014, Xiamen, China, 13/06/14. https://doi.org/10.4028/www.scientific.net/AMM.615.323

Research on inverse system decoupling of three-axis flight simulator based on the high-speed rotation missile. / Yan, Xin Ying; Mo, Bo; Li, Yang Hua.
Automatic Control and Mechatronic Engineering III. Trans Tech Publications Ltd., 2014. p. 323-328 (Applied Mechanics and Materials; Vol. 615).

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

TY - GEN

T1 - Research on inverse system decoupling of three-axis flight simulator based on the high-speed rotation missile

AU - Yan, Xin Ying

AU - Mo, Bo

AU - Li, Yang Hua

PY - 2014

Y1 - 2014

N2 - This paper researches on the kinematics and dynamics of coupling for three-axis flight Simulator based on the high-speed rotation missile. Firstly, to define station body coordinate and the positive direction of rotation according to three-axis flight Simulator based on the high-speed rotation missile, and then the mathematical coupling model is established. Secondly, multivariable nonlinear mathematical model can be decoupling, while substituting the parameters quality attribute analysis solved by ProE into the mathematical model. Lastly, the decoupled linear equations and the decoupling solutions based on inverse system method were given, and then to finish the simulation and to analysis the simulation results.

AB - This paper researches on the kinematics and dynamics of coupling for three-axis flight Simulator based on the high-speed rotation missile. Firstly, to define station body coordinate and the positive direction of rotation according to three-axis flight Simulator based on the high-speed rotation missile, and then the mathematical coupling model is established. Secondly, multivariable nonlinear mathematical model can be decoupling, while substituting the parameters quality attribute analysis solved by ProE into the mathematical model. Lastly, the decoupled linear equations and the decoupling solutions based on inverse system method were given, and then to finish the simulation and to analysis the simulation results.

KW - Decoupling

KW - High-speed rotation missile

KW - Inverse system

KW - Three-axis flight simulator

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U2 - 10.4028/www.scientific.net/AMM.615.323

DO - 10.4028/www.scientific.net/AMM.615.323

M3 - Conference contribution

AN - SCOPUS:84906482841

SN - 9783038351993

T3 - Applied Mechanics and Materials

SP - 323

EP - 328

BT - Automatic Control and Mechatronic Engineering III

PB - Trans Tech Publications Ltd.

T2 - 3rd International Conference on Automatic Control and Mechatronic Engineering, ICACME 2014

Y2 - 13 June 2014 through 14 June 2014

ER -

Research on inverse system decoupling of three-axis flight simulator based on the high-speed rotation missile

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Publication series

Conference

Keywords

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