Miss distance analysis for missiles with lateral jets and aerodynamic surfaces

Yong Tao Bi; Yu Yao; Feng Hua He; Deng Gao Ji

Miss distance analysis for missiles with lateral jets and aerodynamic surfaces

Yong Tao Bi^*
, Yu Yao
, Feng Hua He
, Deng Gao Ji

^*Corresponding author for this work

School of Astronautics

Research output: Contribution to journal › Article › peer-review

Abstract

With consideration of the switch between aerodynamic control and blended control for missiles with lateral jets and aerodynamic surfaces, the relationship between the zero effort miss distance and the parameters of a generic homing guidance system based on finite-time generalized H₂ method was developed. Effects of switch time, effective navigation ratio, amendatory proportional navigation coefficient, and target estimation time constant on the zero effort miss distance were analyzed. The analysis results can provide a basis for determining the switch time of lateral thrust and guidance law parameters.

Original language	English
Pages (from-to)	13-16
Number of pages	4
Journal	Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology
Volume	41
Issue number	11
State	Published - Nov 2009

Keywords

Blended control
Finite-time generalized H method
Lateral thrust
Miss distance analysis

Cite this

@article{ad1037d90f2744d6a86f774b9a93c10e,

title = "Miss distance analysis for missiles with lateral jets and aerodynamic surfaces",

abstract = "With consideration of the switch between aerodynamic control and blended control for missiles with lateral jets and aerodynamic surfaces, the relationship between the zero effort miss distance and the parameters of a generic homing guidance system based on finite-time generalized H2 method was developed. Effects of switch time, effective navigation ratio, amendatory proportional navigation coefficient, and target estimation time constant on the zero effort miss distance were analyzed. The analysis results can provide a basis for determining the switch time of lateral thrust and guidance law parameters.",

keywords = "Blended control, Finite-time generalized H method, Lateral thrust, Miss distance analysis",

author = "Bi, \{Yong Tao\} and Yu Yao and He, \{Feng Hua\} and Ji, \{Deng Gao\}",

year = "2009",

month = nov,

language = "英语",

volume = "41",

pages = "13--16",

journal = "Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology",

issn = "0367-6234",

publisher = "Harbin Institute of Technology",

number = "11",

}

TY - JOUR

T1 - Miss distance analysis for missiles with lateral jets and aerodynamic surfaces

AU - Bi, Yong Tao

AU - Yao, Yu

AU - He, Feng Hua

AU - Ji, Deng Gao

PY - 2009/11

Y1 - 2009/11

N2 - With consideration of the switch between aerodynamic control and blended control for missiles with lateral jets and aerodynamic surfaces, the relationship between the zero effort miss distance and the parameters of a generic homing guidance system based on finite-time generalized H2 method was developed. Effects of switch time, effective navigation ratio, amendatory proportional navigation coefficient, and target estimation time constant on the zero effort miss distance were analyzed. The analysis results can provide a basis for determining the switch time of lateral thrust and guidance law parameters.

AB - With consideration of the switch between aerodynamic control and blended control for missiles with lateral jets and aerodynamic surfaces, the relationship between the zero effort miss distance and the parameters of a generic homing guidance system based on finite-time generalized H2 method was developed. Effects of switch time, effective navigation ratio, amendatory proportional navigation coefficient, and target estimation time constant on the zero effort miss distance were analyzed. The analysis results can provide a basis for determining the switch time of lateral thrust and guidance law parameters.

KW - Blended control

KW - Finite-time generalized H method

KW - Lateral thrust

KW - Miss distance analysis

UR - https://www.scopus.com/pages/publications/74849116380

M3 - 文章

AN - SCOPUS:74849116380

SN - 0367-6234

VL - 41

SP - 13

EP - 16

JO - Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology

JF - Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology

IS - 11

ER -

Miss distance analysis for missiles with lateral jets and aerodynamic surfaces

Abstract

Keywords

Other files and links

Fingerprint

Cite this