H2 control for model helicopter in Hover

Moo Seok Kim; Jopn Ki Kim; Jeong Yup Han; Hong Bae Park; Soon Ju Kang

doi:10.1117/12.664592

H₂ control for model helicopter in Hover

Moo Seok Kim
, Jopn Ki Kim
, Jeong Yup Han
, Hong Bae Park
, Soon Ju Kang

Kyungpook National University

Research output: Contribution to journal › Conference article › peer-review

Abstract

This paper presents mathematical model of six degree-of-freedom (6-DOF) helicopter (ERGO50) in hover, and H₂ feedback controller which is a powerful technique for the MIMO system as a helicopter. Mathematical model of the helicopter is multi-input multi-output (MIMO) and linearized system which accommodates aerodynamics. H₂ controller based on optimal control theory is used in a myriad application and plays an important role as a valuable precursor to other advanced methods for future work, when we need to improve stability of the helicopter. We design linear-quadratic-gaussian controller as H₂ controller. Simulation results show good performance.

Original language	English
Article number	604215
Journal	Proceedings of SPIE - The International Society for Optical Engineering
Volume	6042 I
DOIs	https://doi.org/10.1117/12.664592
State	Published - 2005
Event	ICMIT 2005: Control Systems and Robotics - Chongging, China Duration: 20 Sep 2005 → 23 Sep 2005

Keywords

6-DOF mathematical model
Aerodynamic
H controller
Linearized system
LQG
LTR
MIMO

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10.1117/12.664592

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title = "H2 control for model helicopter in Hover",

abstract = "This paper presents mathematical model of six degree-of-freedom (6-DOF) helicopter (ERGO50) in hover, and H2 feedback controller which is a powerful technique for the MIMO system as a helicopter. Mathematical model of the helicopter is multi-input multi-output (MIMO) and linearized system which accommodates aerodynamics. H2 controller based on optimal control theory is used in a myriad application and plays an important role as a valuable precursor to other advanced methods for future work, when we need to improve stability of the helicopter. We design linear-quadratic-gaussian controller as H2 controller. Simulation results show good performance.",

keywords = "6-DOF mathematical model, Aerodynamic, H controller, Linearized system, LQG, LTR, MIMO",

author = "Kim, \{Moo Seok\} and Kim, \{Jopn Ki\} and Han, \{Jeong Yup\} and Park, \{Hong Bae\} and Kang, \{Soon Ju\}",

year = "2005",

doi = "10.1117/12.664592",

language = "English",

volume = "6042 I",

journal = "Proceedings of SPIE - The International Society for Optical Engineering",

issn = "0277-786X",

publisher = "SPIE",

note = "ICMIT 2005: Control Systems and Robotics ; Conference date: 20-09-2005 Through 23-09-2005",

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TY - JOUR

T1 - H2 control for model helicopter in Hover

AU - Kim, Moo Seok

AU - Kim, Jopn Ki

AU - Han, Jeong Yup

AU - Park, Hong Bae

AU - Kang, Soon Ju

PY - 2005

Y1 - 2005

N2 - This paper presents mathematical model of six degree-of-freedom (6-DOF) helicopter (ERGO50) in hover, and H2 feedback controller which is a powerful technique for the MIMO system as a helicopter. Mathematical model of the helicopter is multi-input multi-output (MIMO) and linearized system which accommodates aerodynamics. H2 controller based on optimal control theory is used in a myriad application and plays an important role as a valuable precursor to other advanced methods for future work, when we need to improve stability of the helicopter. We design linear-quadratic-gaussian controller as H2 controller. Simulation results show good performance.

AB - This paper presents mathematical model of six degree-of-freedom (6-DOF) helicopter (ERGO50) in hover, and H2 feedback controller which is a powerful technique for the MIMO system as a helicopter. Mathematical model of the helicopter is multi-input multi-output (MIMO) and linearized system which accommodates aerodynamics. H2 controller based on optimal control theory is used in a myriad application and plays an important role as a valuable precursor to other advanced methods for future work, when we need to improve stability of the helicopter. We design linear-quadratic-gaussian controller as H2 controller. Simulation results show good performance.

KW - 6-DOF mathematical model

KW - Aerodynamic

KW - H controller

KW - Linearized system

KW - LQG

KW - LTR

KW - MIMO

UR - https://www.scopus.com/pages/publications/33646518530

U2 - 10.1117/12.664592

DO - 10.1117/12.664592

M3 - Conference article

AN - SCOPUS:33646518530

SN - 0277-786X

VL - 6042 I

JO - Proceedings of SPIE - The International Society for Optical Engineering

JF - Proceedings of SPIE - The International Society for Optical Engineering

M1 - 604215

T2 - ICMIT 2005: Control Systems and Robotics

Y2 - 20 September 2005 through 23 September 2005

ER -

H₂ control for model helicopter in Hover

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Keywords

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