Computing stability for autopilots based on vector margin

Jiang Wang; De Fu Lin; Jun Fang Fan

doi:10.1007/978-3-642-31003-4_58

Computing stability for autopilots based on vector margin

Jiang Wang^*, De Fu Lin, Jun Fang Fan

^*此作品的通讯作者

宇航学院

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

摘要

A novel stability computation approach for tactical missile autopilots was detailed. The limitations of traditional stability margins were exhibited. Then the vector margin was introduced and examined. All available linear autopilot topologies were given and evaluated on the basis of vector margin. The analysis and computation results show that the presented method could give well description for control system stability.

源语言	英语
主期刊名	Future Control and Automation - Proceedings of the 2nd International Conference on Future Control and Automation, ICFCA 2012
页	455-460
页数	6
版本	VOL. 2
DOI	https://doi.org/10.1007/978-3-642-31003-4_58
出版状态	已出版 - 2012
活动	2nd International Conference on Future Control and Automation, ICFCA 2012 - Changsha, 中国期限: 1 7月 2012 → 2 7月 2012

出版系列

姓名	Lecture Notes in Electrical Engineering
编号	VOL. 2
卷	173 LNEE
ISSN（印刷版）	1876-1100
ISSN（电子版）	1876-1119

会议

会议	2nd International Conference on Future Control and Automation, ICFCA 2012
国家/地区	中国
市	Changsha
时期	1/07/12 → 2/07/12

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10.1007/978-3-642-31003-4_58

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引用此

Wang, J., Lin, D. F., & Fan, J. F. (2012). Computing stability for autopilots based on vector margin. 在 Future Control and Automation - Proceedings of the 2nd International Conference on Future Control and Automation, ICFCA 2012 (VOL. 2 编辑, 页码 455-460). (Lecture Notes in Electrical Engineering; 卷 173 LNEE, 号码 VOL. 2). https://doi.org/10.1007/978-3-642-31003-4_58

@inproceedings{3da3b5dd248548bd8914c6bcce1cbd62,

title = "Computing stability for autopilots based on vector margin",

abstract = "A novel stability computation approach for tactical missile autopilots was detailed. The limitations of traditional stability margins were exhibited. Then the vector margin was introduced and examined. All available linear autopilot topologies were given and evaluated on the basis of vector margin. The analysis and computation results show that the presented method could give well description for control system stability.",

keywords = "autopilot, stability computation, vector margin",

author = "Jiang Wang and Lin, {De Fu} and Fan, {Jun Fang}",

year = "2012",

doi = "10.1007/978-3-642-31003-4_58",

language = "English",

isbn = "9783642310027",

series = "Lecture Notes in Electrical Engineering",

number = "VOL. 2",

pages = "455--460",

booktitle = "Future Control and Automation - Proceedings of the 2nd International Conference on Future Control and Automation, ICFCA 2012",

edition = "VOL. 2",

note = "2nd International Conference on Future Control and Automation, ICFCA 2012 ; Conference date: 01-07-2012 Through 02-07-2012",

}

Wang, J, Lin, DF & Fan, JF 2012, Computing stability for autopilots based on vector margin. 在 Future Control and Automation - Proceedings of the 2nd International Conference on Future Control and Automation, ICFCA 2012. VOL. 2 编辑, Lecture Notes in Electrical Engineering, 号码 VOL. 2, 卷 173 LNEE, 页码 455-460, 2nd International Conference on Future Control and Automation, ICFCA 2012, Changsha, 中国, 1/07/12. https://doi.org/10.1007/978-3-642-31003-4_58

Computing stability for autopilots based on vector margin. / Wang, Jiang; Lin, De Fu; Fan, Jun Fang.
Future Control and Automation - Proceedings of the 2nd International Conference on Future Control and Automation, ICFCA 2012. VOL. 2. 编辑 2012. 页码 455-460 (Lecture Notes in Electrical Engineering; 卷 173 LNEE, 号码 VOL. 2).

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

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T1 - Computing stability for autopilots based on vector margin

AU - Wang, Jiang

AU - Lin, De Fu

AU - Fan, Jun Fang

PY - 2012

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N2 - A novel stability computation approach for tactical missile autopilots was detailed. The limitations of traditional stability margins were exhibited. Then the vector margin was introduced and examined. All available linear autopilot topologies were given and evaluated on the basis of vector margin. The analysis and computation results show that the presented method could give well description for control system stability.

AB - A novel stability computation approach for tactical missile autopilots was detailed. The limitations of traditional stability margins were exhibited. Then the vector margin was introduced and examined. All available linear autopilot topologies were given and evaluated on the basis of vector margin. The analysis and computation results show that the presented method could give well description for control system stability.

KW - autopilot

KW - stability computation

KW - vector margin

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DO - 10.1007/978-3-642-31003-4_58

M3 - Conference contribution

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SN - 9783642310027

T3 - Lecture Notes in Electrical Engineering

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EP - 460

BT - Future Control and Automation - Proceedings of the 2nd International Conference on Future Control and Automation, ICFCA 2012

T2 - 2nd International Conference on Future Control and Automation, ICFCA 2012

Y2 - 1 July 2012 through 2 July 2012

ER -

Computing stability for autopilots based on vector margin

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