Missile autopilot design using optimal control and frequency constraint

Fan Jun-Fang; Lin De-Fu; Qi Zai-Kang; Wang Jiang

doi:10.1109/ISSCAA.2008.4776240

Missile autopilot design using optimal control and frequency constraint

Fan Jun-Fang^*, Lin De-Fu, Qi Zai-Kang, Wang Jiang

^*此作品的通讯作者

宇航学院

Beijing Institute of Technology

科研成果: 会议稿件 › 论文 › 同行评审

3 引用（Scopus）

摘要

The benefits of relaxed static stability on missile were examined. Based on optimal control and open-loop crossover frequency constraint, an acceleration autopilot design methodology was developed and applied to a highly unstable airframe. Performance and robustness comparisons for three autopilot topologies were made. The analysis reveals the topology origin of classic three-loop autopilot, and simulation results show that the four-loop topology looks very promising.

源语言	英语
DOI	https://doi.org/10.1109/ISSCAA.2008.4776240
出版状态	已出版 - 2008
活动	2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics, ISSCAA 2008 - Shenzhen, 中国期限: 10 12月 2008 → 12 12月 2008

会议

会议	2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics, ISSCAA 2008
国家/地区	中国
市	Shenzhen
时期	10/12/08 → 12/12/08

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10.1109/ISSCAA.2008.4776240

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链接到 Scopus 的出版物

引用此

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title = "Missile autopilot design using optimal control and frequency constraint",

abstract = "The benefits of relaxed static stability on missile were examined. Based on optimal control and open-loop crossover frequency constraint, an acceleration autopilot design methodology was developed and applied to a highly unstable airframe. Performance and robustness comparisons for three autopilot topologies were made. The analysis reveals the topology origin of classic three-loop autopilot, and simulation results show that the four-loop topology looks very promising.",

keywords = "Autopilot, Frequency constraint, Optimal control, Optimization, Static unstable missile",

author = "Fan Jun-Fang and Lin De-Fu and Qi Zai-Kang and Wang Jiang",

year = "2008",

doi = "10.1109/ISSCAA.2008.4776240",

language = "English",

note = "2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics, ISSCAA 2008 ; Conference date: 10-12-2008 Through 12-12-2008",

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TY - CONF

T1 - Missile autopilot design using optimal control and frequency constraint

AU - Jun-Fang, Fan

AU - De-Fu, Lin

AU - Zai-Kang, Qi

AU - Jiang, Wang

PY - 2008

Y1 - 2008

N2 - The benefits of relaxed static stability on missile were examined. Based on optimal control and open-loop crossover frequency constraint, an acceleration autopilot design methodology was developed and applied to a highly unstable airframe. Performance and robustness comparisons for three autopilot topologies were made. The analysis reveals the topology origin of classic three-loop autopilot, and simulation results show that the four-loop topology looks very promising.

AB - The benefits of relaxed static stability on missile were examined. Based on optimal control and open-loop crossover frequency constraint, an acceleration autopilot design methodology was developed and applied to a highly unstable airframe. Performance and robustness comparisons for three autopilot topologies were made. The analysis reveals the topology origin of classic three-loop autopilot, and simulation results show that the four-loop topology looks very promising.

KW - Autopilot

KW - Frequency constraint

KW - Optimal control

KW - Optimization

KW - Static unstable missile

UR - http://www.scopus.com/inward/record.url?scp=66449125290&partnerID=8YFLogxK

U2 - 10.1109/ISSCAA.2008.4776240

DO - 10.1109/ISSCAA.2008.4776240

M3 - Paper

AN - SCOPUS:66449125290

T2 - 2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics, ISSCAA 2008

Y2 - 10 December 2008 through 12 December 2008

ER -

Missile autopilot design using optimal control and frequency constraint

摘要

会议

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