Design and analysis of missile two-loop autopilot with PI compensator under multi-constraints

Hui Wang; De Fu Lin; Jiang Wang; Zhen Xuan Cheng

doi:10.1109/ICACTE.2010.5579274

Design and analysis of missile two-loop autopilot with PI compensator under multi-constraints

Hui Wang^*, De Fu Lin, Jiang Wang, Zhen Xuan Cheng

^*Corresponding author for this work

School of Aerospace Engineering

Academy of Ordnance Science

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

4 Citations (Scopus)

Abstract

In order to eliminate the static error, PI compensator was introduced to the classic two-loop autopilot and the contribution of PI was analyzed while the equivalent time constant estimates of two-loop autopilot with PI was discussed. Four different objective functions were introduced to the design procedures. It is concluded that it is the large gain at low frequency of PI solved the problem of static error.

Original language	English
Title of host publication	ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings
Pages	V5117-V5121
DOIs	https://doi.org/10.1109/ICACTE.2010.5579274
Publication status	Published - 2010
Event	2010 3rd International Conference on Advanced Computer Theory and Engineering, ICACTE 2010 - Chengdu, China Duration: 20 Aug 2010 → 22 Aug 2010

Publication series

Name	ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings
Volume	5

Conference

Conference	2010 3rd International Conference on Advanced Computer Theory and Engineering, ICACTE 2010
Country/Territory	China
City	Chengdu
Period	20/08/10 → 22/08/10

Keywords

Autopilot
Missile
Objective function
PI compensator
State feedback

Access to Document

10.1109/ICACTE.2010.5579274

Cite this

Wang, H., Lin, D. F., Wang, J., & Cheng, Z. X. (2010). Design and analysis of missile two-loop autopilot with PI compensator under multi-constraints. In ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings (pp. V5117-V5121). Article 5579274 (ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings; Vol. 5). https://doi.org/10.1109/ICACTE.2010.5579274

Wang, Hui ; Lin, De Fu ; Wang, Jiang et al. / Design and analysis of missile two-loop autopilot with PI compensator under multi-constraints. ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings. 2010. pp. V5117-V5121 (ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings).

@inproceedings{db4557b47a4c4429aad44d4f465157bc,

title = "Design and analysis of missile two-loop autopilot with PI compensator under multi-constraints",

abstract = "In order to eliminate the static error, PI compensator was introduced to the classic two-loop autopilot and the contribution of PI was analyzed while the equivalent time constant estimates of two-loop autopilot with PI was discussed. Four different objective functions were introduced to the design procedures. It is concluded that it is the large gain at low frequency of PI solved the problem of static error.",

keywords = "Autopilot, Missile, Objective function, PI compensator, State feedback",

author = "Hui Wang and Lin, \{De Fu\} and Jiang Wang and Cheng, \{Zhen Xuan\}",

year = "2010",

doi = "10.1109/ICACTE.2010.5579274",

language = "English",

isbn = "9781424465408",

series = "ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings",

pages = "V5117--V5121",

booktitle = "ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings",

note = "2010 3rd International Conference on Advanced Computer Theory and Engineering, ICACTE 2010 ; Conference date: 20-08-2010 Through 22-08-2010",

}

Wang, H , Lin, DF , Wang, J & Cheng, ZX 2010, Design and analysis of missile two-loop autopilot with PI compensator under multi-constraints. in ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings., 5579274, ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings, vol. 5, pp. V5117-V5121, 2010 3rd International Conference on Advanced Computer Theory and Engineering, ICACTE 2010, Chengdu, China, 20/08/10. https://doi.org/10.1109/ICACTE.2010.5579274

Design and analysis of missile two-loop autopilot with PI compensator under multi-constraints. / Wang, Hui ; Lin, De Fu ; Wang, Jiang et al.
ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings. 2010. p. V5117-V5121 5579274 (ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings; Vol. 5).

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

TY - GEN

T1 - Design and analysis of missile two-loop autopilot with PI compensator under multi-constraints

AU - Wang, Hui

AU - Lin, De Fu

AU - Wang, Jiang

AU - Cheng, Zhen Xuan

PY - 2010

Y1 - 2010

N2 - In order to eliminate the static error, PI compensator was introduced to the classic two-loop autopilot and the contribution of PI was analyzed while the equivalent time constant estimates of two-loop autopilot with PI was discussed. Four different objective functions were introduced to the design procedures. It is concluded that it is the large gain at low frequency of PI solved the problem of static error.

AB - In order to eliminate the static error, PI compensator was introduced to the classic two-loop autopilot and the contribution of PI was analyzed while the equivalent time constant estimates of two-loop autopilot with PI was discussed. Four different objective functions were introduced to the design procedures. It is concluded that it is the large gain at low frequency of PI solved the problem of static error.

KW - Autopilot

KW - Missile

KW - Objective function

KW - PI compensator

KW - State feedback

UR - https://www.scopus.com/pages/publications/78149308443

U2 - 10.1109/ICACTE.2010.5579274

DO - 10.1109/ICACTE.2010.5579274

M3 - Conference contribution

AN - SCOPUS:78149308443

SN - 9781424465408

T3 - ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings

SP - V5117-V5121

BT - ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings

T2 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, ICACTE 2010

Y2 - 20 August 2010 through 22 August 2010

ER -

Wang H , Lin DF , Wang J, Cheng ZX. Design and analysis of missile two-loop autopilot with PI compensator under multi-constraints. In ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings. 2010. p. V5117-V5121. 5579274. (ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings). doi: 10.1109/ICACTE.2010.5579274

Design and analysis of missile two-loop autopilot with PI compensator under multi-constraints

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