Research of integrative GNC design simulation for cruise missile

Bo Yang; Qiuxia Hu; Hanmei Wang

doi:10.1109/WGEC.2009.88

Research of integrative GNC design simulation for cruise missile

Bo Yang^*
, Qiuxia Hu
, Hanmei Wang

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Beihang University

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

Abstract

Scheme guidance is widely used in the gaining altitude phase and level flight phase of cruise missile. The missile aviates according to the planed procedure, but the unchanged scheme can't adapt to the large diversification which will possibly occur in flight, and will result in a long time' response. This paper brings forward a design method of integrative GNC, which combines the navigation information with the scheme component. In certain conditions, the scheme component will start up flexible flight procedure, meanwhile transfer the manipulative parameters into the ones which are fit the real-time situation, and end in the smooth transition between scheduled aim and provisional flight path.

Original language	English
Title of host publication	3rd International Conference on Genetic and Evolutionary Computing, WGEC 2009
Pages	397-401
Number of pages	5
DOIs	https://doi.org/10.1109/WGEC.2009.88
State	Published - 2009
Event	3rd International Conference on Genetic and Evolutionary Computing, WGEC 2009 - Guilin, China Duration: 14 Oct 2009 → 17 Oct 2009

Publication series

Name	3rd International Conference on Genetic and Evolutionary Computing, WGEC 2009

Conference

Conference	3rd International Conference on Genetic and Evolutionary Computing, WGEC 2009
Country/Territory	China
City	Guilin
Period	14/10/09 → 17/10/09

Keywords

Cruise missile
Integrative GNC

Access to Document

10.1109/WGEC.2009.88

Cite this

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title = "Research of integrative GNC design simulation for cruise missile",

abstract = "Scheme guidance is widely used in the gaining altitude phase and level flight phase of cruise missile. The missile aviates according to the planed procedure, but the unchanged scheme can't adapt to the large diversification which will possibly occur in flight, and will result in a long time' response. This paper brings forward a design method of integrative GNC, which combines the navigation information with the scheme component. In certain conditions, the scheme component will start up flexible flight procedure, meanwhile transfer the manipulative parameters into the ones which are fit the real-time situation, and end in the smooth transition between scheduled aim and provisional flight path.",

keywords = "Cruise missile, Integrative GNC",

author = "Bo Yang and Qiuxia Hu and Hanmei Wang",

year = "2009",

doi = "10.1109/WGEC.2009.88",

language = "英语",

isbn = "9780769538990",

series = "3rd International Conference on Genetic and Evolutionary Computing, WGEC 2009",

pages = "397--401",

booktitle = "3rd International Conference on Genetic and Evolutionary Computing, WGEC 2009",

note = "3rd International Conference on Genetic and Evolutionary Computing, WGEC 2009 ; Conference date: 14-10-2009 Through 17-10-2009",

}

Yang, B, Hu, Q & Wang, H 2009, Research of integrative GNC design simulation for cruise missile. in 3rd International Conference on Genetic and Evolutionary Computing, WGEC 2009., 5402864, 3rd International Conference on Genetic and Evolutionary Computing, WGEC 2009, pp. 397-401, 3rd International Conference on Genetic and Evolutionary Computing, WGEC 2009, Guilin, China, 14/10/09. https://doi.org/10.1109/WGEC.2009.88

Research of integrative GNC design simulation for cruise missile. / Yang, Bo; Hu, Qiuxia; Wang, Hanmei.
3rd International Conference on Genetic and Evolutionary Computing, WGEC 2009. 2009. p. 397-401 5402864 (3rd International Conference on Genetic and Evolutionary Computing, WGEC 2009).

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

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T1 - Research of integrative GNC design simulation for cruise missile

AU - Yang, Bo

AU - Hu, Qiuxia

AU - Wang, Hanmei

PY - 2009

Y1 - 2009

N2 - Scheme guidance is widely used in the gaining altitude phase and level flight phase of cruise missile. The missile aviates according to the planed procedure, but the unchanged scheme can't adapt to the large diversification which will possibly occur in flight, and will result in a long time' response. This paper brings forward a design method of integrative GNC, which combines the navigation information with the scheme component. In certain conditions, the scheme component will start up flexible flight procedure, meanwhile transfer the manipulative parameters into the ones which are fit the real-time situation, and end in the smooth transition between scheduled aim and provisional flight path.

AB - Scheme guidance is widely used in the gaining altitude phase and level flight phase of cruise missile. The missile aviates according to the planed procedure, but the unchanged scheme can't adapt to the large diversification which will possibly occur in flight, and will result in a long time' response. This paper brings forward a design method of integrative GNC, which combines the navigation information with the scheme component. In certain conditions, the scheme component will start up flexible flight procedure, meanwhile transfer the manipulative parameters into the ones which are fit the real-time situation, and end in the smooth transition between scheduled aim and provisional flight path.

KW - Cruise missile

KW - Integrative GNC

UR - https://www.scopus.com/pages/publications/77950677689

U2 - 10.1109/WGEC.2009.88

DO - 10.1109/WGEC.2009.88

M3 - 会议稿件

AN - SCOPUS:77950677689

SN - 9780769538990

T3 - 3rd International Conference on Genetic and Evolutionary Computing, WGEC 2009

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BT - 3rd International Conference on Genetic and Evolutionary Computing, WGEC 2009

T2 - 3rd International Conference on Genetic and Evolutionary Computing, WGEC 2009

Y2 - 14 October 2009 through 17 October 2009

ER -

Research of integrative GNC design simulation for cruise missile

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Keywords

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