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

^*Corresponding author for this work

School of Aerospace Engineering

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

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.

Original language	English
Title of host publication	Future Control and Automation - Proceedings of the 2nd International Conference on Future Control and Automation, ICFCA 2012
Pages	455-460
Number of pages	6
Edition	VOL. 2
DOIs	https://doi.org/10.1007/978-3-642-31003-4_58
Publication status	Published - 2012
Event	2nd International Conference on Future Control and Automation, ICFCA 2012 - Changsha, China Duration: 1 Jul 2012 → 2 Jul 2012

Publication series

Name	Lecture Notes in Electrical Engineering
Number	VOL. 2
Volume	173 LNEE
ISSN (Print)	1876-1100
ISSN (Electronic)	1876-1119

Conference

Conference	2nd International Conference on Future Control and Automation, ICFCA 2012
Country/Territory	China
City	Changsha
Period	1/07/12 → 2/07/12

Keywords

autopilot
stability computation
vector margin

Access to Document

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

Cite this

Wang, J., Lin, D. F., & Fan, J. F. (2012). Computing stability for autopilots based on vector margin. In Future Control and Automation - Proceedings of the 2nd International Conference on Future Control and Automation, ICFCA 2012 (VOL. 2 ed., pp. 455-460). (Lecture Notes in Electrical Engineering; Vol. 173 LNEE, No. 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. in Future Control and Automation - Proceedings of the 2nd International Conference on Future Control and Automation, ICFCA 2012. VOL. 2 edn, Lecture Notes in Electrical Engineering, no. VOL. 2, vol. 173 LNEE, pp. 455-460, 2nd International Conference on Future Control and Automation, ICFCA 2012, Changsha, China, 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. ed. 2012. p. 455-460 (Lecture Notes in Electrical Engineering; Vol. 173 LNEE, No. VOL. 2).

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

TY - GEN

T1 - Computing stability for autopilots based on vector margin

AU - Wang, Jiang

AU - Lin, De Fu

AU - Fan, Jun Fang

PY - 2012

Y1 - 2012

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

UR - http://www.scopus.com/inward/record.url?scp=84865973638&partnerID=8YFLogxK

U2 - 10.1007/978-3-642-31003-4_58

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

M3 - Conference contribution

AN - SCOPUS:84865973638

SN - 9783642310027

T3 - Lecture Notes in Electrical Engineering

SP - 455

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

Abstract

Publication series

Conference

Keywords

Access to Document

Other files and links

Fingerprint

Cite this