MULTIVARIABLE CONTROL OF A TWIN LIFT HELICOPTER SYSTEM USING THE LQG/LTR DESIGN METHODOLOGY.

Armando Rodriguez; Michael Athans

MULTIVARIABLE CONTROL OF A TWIN LIFT HELICOPTER SYSTEM USING THE LQG/LTR DESIGN METHODOLOGY.

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

Abstract

Guidelines are presented for developing a multivariable, centralized automatic flight control system for a twin lift helicopter system. Singular value ideas are used to formulate performance and stability robustness specifications. A linear-quadratic-Gaussian with loop-transfer-recovery (LQG/LTR) design is obtained and evaluated.

Original language	English (US)
Title of host publication	Proceedings of the American Control Conference
Publisher	IEEE
Pages	1325-1332
Number of pages	8
State	Published - 1986
Externally published	Yes

ASJC Scopus subject areas

Control and Systems Engineering

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@inproceedings{ff90ab48586143c4ab05032ecd584de4,

title = "MULTIVARIABLE CONTROL OF A TWIN LIFT HELICOPTER SYSTEM USING THE LQG/LTR DESIGN METHODOLOGY.",

abstract = "Guidelines are presented for developing a multivariable, centralized automatic flight control system for a twin lift helicopter system. Singular value ideas are used to formulate performance and stability robustness specifications. A linear-quadratic-Gaussian with loop-transfer-recovery (LQG/LTR) design is obtained and evaluated.",

author = "Armando Rodriguez and Michael Athans",

year = "1986",

language = "English (US)",

pages = "1325--1332",

booktitle = "Proceedings of the American Control Conference",

publisher = "IEEE",

}

TY - GEN

T1 - MULTIVARIABLE CONTROL OF A TWIN LIFT HELICOPTER SYSTEM USING THE LQG/LTR DESIGN METHODOLOGY.

AU - Rodriguez, Armando

AU - Athans, Michael

PY - 1986

Y1 - 1986

N2 - Guidelines are presented for developing a multivariable, centralized automatic flight control system for a twin lift helicopter system. Singular value ideas are used to formulate performance and stability robustness specifications. A linear-quadratic-Gaussian with loop-transfer-recovery (LQG/LTR) design is obtained and evaluated.

AB - Guidelines are presented for developing a multivariable, centralized automatic flight control system for a twin lift helicopter system. Singular value ideas are used to formulate performance and stability robustness specifications. A linear-quadratic-Gaussian with loop-transfer-recovery (LQG/LTR) design is obtained and evaluated.

UR - http://www.scopus.com/inward/record.url?scp=0022605824&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=0022605824&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:0022605824

SP - 1325

EP - 1332

BT - Proceedings of the American Control Conference

PB - IEEE

ER -

MULTIVARIABLE CONTROL OF A TWIN LIFT HELICOPTER SYSTEM USING THE LQG/LTR DESIGN METHODOLOGY.

Abstract

ASJC Scopus subject areas

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