A new precision analysis method for missile attitude control system with parametric perturbation

Ruimin Jiang; Jun Zhou; Jianguo Guo; Guoqing Wang

A new precision analysis method for missile attitude control system with parametric perturbation

Ruimin Jiang
, Jun Zhou
, Jianguo Guo
, Guoqing Wang

航天学院

Northwestern Polytechnical University Xian
China Aerospace Science and Technology Corporation

科研成果: 期刊稿件 › 文章 › 同行评审

3 引用（Scopus）

摘要

Covariance Analysis Describing Function Technique (CADET) is considered too crude for precision analysis of systems with parametric perturbation. We present new precision analysis method for missile attitude control system with parametric perturbation considered. Based on the traditional CADET method, the generalized nonlinear part including parametric perturbation is statistically linearized. The differential equations of state mean and covariance are obtained. We simulate a missile attitude control system, using respectively modified CADET method and Monte Carlo method. The results and their analysis show preliminarily that modified CADET method can indeed analyze the precision of missile attitude control system with both disturbance and parametric perturbation.

源语言	英语
页（从-至）	560-564
页数	5
期刊	Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University
卷	31
期	4
出版状态	已出版 - 2013

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title = "A new precision analysis method for missile attitude control system with parametric perturbation",

abstract = "Covariance Analysis Describing Function Technique (CADET) is considered too crude for precision analysis of systems with parametric perturbation. We present new precision analysis method for missile attitude control system with parametric perturbation considered. Based on the traditional CADET method, the generalized nonlinear part including parametric perturbation is statistically linearized. The differential equations of state mean and covariance are obtained. We simulate a missile attitude control system, using respectively modified CADET method and Monte Carlo method. The results and their analysis show preliminarily that modified CADET method can indeed analyze the precision of missile attitude control system with both disturbance and parametric perturbation.",

keywords = "Attitude control, Differential equations, Mathematical models, Modified CADET (covariance analysis describing function technique), Monte Carlo methods, Parametric perturbation, Precision analysis, Sliding mode control, Statistical methods, Uncertain systems, Variable structure control",

author = "Ruimin Jiang and Jun Zhou and Jianguo Guo and Guoqing Wang",

year = "2013",

language = "英语",

volume = "31",

pages = "560--564",

journal = "Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University",

issn = "1000-2758",

publisher = "Northwestern Polytechnical University",

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TY - JOUR

T1 - A new precision analysis method for missile attitude control system with parametric perturbation

AU - Jiang, Ruimin

AU - Zhou, Jun

AU - Guo, Jianguo

AU - Wang, Guoqing

PY - 2013

Y1 - 2013

N2 - Covariance Analysis Describing Function Technique (CADET) is considered too crude for precision analysis of systems with parametric perturbation. We present new precision analysis method for missile attitude control system with parametric perturbation considered. Based on the traditional CADET method, the generalized nonlinear part including parametric perturbation is statistically linearized. The differential equations of state mean and covariance are obtained. We simulate a missile attitude control system, using respectively modified CADET method and Monte Carlo method. The results and their analysis show preliminarily that modified CADET method can indeed analyze the precision of missile attitude control system with both disturbance and parametric perturbation.

AB - Covariance Analysis Describing Function Technique (CADET) is considered too crude for precision analysis of systems with parametric perturbation. We present new precision analysis method for missile attitude control system with parametric perturbation considered. Based on the traditional CADET method, the generalized nonlinear part including parametric perturbation is statistically linearized. The differential equations of state mean and covariance are obtained. We simulate a missile attitude control system, using respectively modified CADET method and Monte Carlo method. The results and their analysis show preliminarily that modified CADET method can indeed analyze the precision of missile attitude control system with both disturbance and parametric perturbation.

KW - Attitude control

KW - Differential equations

KW - Mathematical models

KW - Modified CADET (covariance analysis describing function technique)

KW - Monte Carlo methods

KW - Parametric perturbation

KW - Precision analysis

KW - Sliding mode control

KW - Statistical methods

KW - Uncertain systems

KW - Variable structure control

UR - https://www.scopus.com/pages/publications/84886252864

M3 - 文章

AN - SCOPUS:84886252864

SN - 1000-2758

VL - 31

SP - 560

EP - 564

JO - Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University

JF - Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University

IS - 4

ER -

A new precision analysis method for missile attitude control system with parametric perturbation

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