LIGO-G030187-00-DPage 1 Modal Analysis and Feedback Control of HAM MEPI Oct 16, 2002 Lei Zuo Osamah Rifai Samir Nayfeh.

Slides:



Advertisements
Similar presentations
FINAL FOCUS: COMBINATION OF PRE ISOLATOR AND ACTIVE STABILISATION K. Artoos, C. Collette, R. Leuxe, C.Eymin, P. Fernandez, S. Janssens * The research leading.
Advertisements

Stability Margins Professor Walter W. Olson
Frequency response When a linear system is subjected to a sinusoidal input, its steady state response is also a sustained sinusoidal wave, with the same.
Decentralized Control Applied to Multi-DOF Tuned-Mass Damper Design Decentralized H2 Control Decentralized H  Control Decentralized Pole Shifting Decentralized.
Takanori Sekiguchi Italy-Japan Workshop (19 April, 2013) Inverted Pendulum Control for KAGRA Seismic Attenuation System 1 D2, Institute for Cosmic Ray.
Loop Shaping Professor Walter W. Olson
Flexures for Optics. Outline Brief overviews of micro flexures Focus on macro flexures in this tutorial Beam bending Symmetry -> precision Degree of freedom.
LIGO-G D 1 Coupled Dynamics of Payload Structures on the Seismically Isolated Optics Table Dennis Coyne, LIGO Caltech SWG Meeting, 2 Sep 2005.
Chapter 8 Root Locus and Magnitude-phase Representation
A Typical Feedback System
LIGO-G D Evaluation of EPI Approaches Dennis Coyne 18 April 2003 EPI Design Review #2.
Active Suspension System Test Platform – Controls Advisor: Mr. Steven Gutschlag Presented: 29 April 2004 Project Member: Jerry L. Campbell Senior Presentation.
Gain margin and phase margin Closed-loop gain of amplifiers with feedback is replacing s=j2πf gives the closed loop gain as a function of frequency For.
G M Advanced R&D1 Seismic Isolation Retrofit Plan for the LIGO Livingston Observatory Dennis Coyne 29 Nov 2001.
Frequency Response Methods and Stability
LIGO Magnetic External Pre-Isolator Richard Mittleman, David Ottaway & Gregg Harry April 18, 2003.
I. Concepts and Tools Mathematics for Dynamic Systems Time Response
RF Stability Working Group Jorn Jacob (ESRF), John Byrd (LBNL) General Issues RF phase and amplitude noise –filtered by cavity and translate into timing.
Dr. / Mohamed Ahmed Ebrahim Mohamed Automatic Control By Dr. / Mohamed Ahmed Ebrahim Mohamed Web site:
Multivariable systems Relative Gain Array (RGA)
Chapter 4: Feedback Control System Characteristics Objectives
Multivariable Control Systems
1 Basic Control Theory and Its Application in AMB Systems Zongli Lin University of Virginia.
EE136 STABILITY AND CONTROL LOOP COMPENSATION IN SWITCH MODE POWER SUPPLY Present By Huyen Tran.
Effects of the cryogenics operational conditions on the mechanical stability of the FLASH linac modules Ramila Amirikas, Alessandro Bertolini, Jürgen Eschke,
Small Signal Stability Analysis Study: study prepared by Powertech Labs Inc. for ERCOT Vance Beauregard AEP 9 April 2002.
Takanori Sekiguchi External Review Alignment control servo for type-B/type-Bp (OpLev/WFS) 1 T. Sekiguchi.
Frequency Response OBJECTIVE - Bode and Nyquist plots for control analysis - Determination of transfer function - Gain and Phase margins - Stability in.
Professor Walter W. Olson Department of Mechanical, Industrial and Manufacturing Engineering University of Toledo Loop Shaping.
Institute of Flight Mechanics and Control Barcelona, LISA7 Symposium, June 17th 2008 IFR – University of Stuttgart LISA Pathfinder.
Seismic Attenuation System (SAS) for LCGT Inverted pendulum: 30mHz 3 cascaded GAS filter: 500mHz Test mass suspension: triple pendulum Transfer functions.
Takanori Sekiguchi External Review Control and tuning of suspension 1 T. Sekiguchi KAGRA 4th External Review.
The purpose of the change of basis matrices is to combine local instruments to sense (or drive ) the platforms rigid body motions along the axis of the.
Structural Dynamics & Vibration Control Lab. 1 Kang-Min Choi, Ph.D. Candidate, KAIST, Korea Jung-Hyun Hong, Graduate Student, KAIST, Korea Ji-Seong Jo,
INC 341PT & BP INC341 Frequency Response Method (continue) Lecture 12.
Chapter 14 Frequency Response Force dynamic process with A sin  t, Chapter
EWEC 2007, MilanoMartin Geyler 1 Individual Blade Pitch Control Design for Load Reduction on Large Wind Turbines EWEC 2007 Milano, 7-10 May 2007 Martin.
Frequency Response OBJECTIVE - Bode and Nyquist plots for control analysis - Determination of transfer function - Gain and Phase margins - Stability in.
HAM-SAS fabrication weekly CALTECH, 4/26/06 V. Boschi, V. Sannibale HAM-SAS Mechanical Model Present Status.
An Introduction to Rotorcraft Dynamics
Professor Walter W. Olson Department of Mechanical, Industrial and Manufacturing Engineering University of Toledo Sensitivity.
1 Decentralized control Sigurd Skogestad Department of Chemical Engineering Norwegian University of Science and Tecnology (NTNU) Trondheim, Norway.
Chapter 6: Frequency Domain Anaysis
DC-DC Fundamentals 1.5 Converter Control. What is Converter Control? A converter can provide a constant voltage output at various condition because of.
Hard or Soft ? C. Collette, K. Artoos, S. Janssens, P. Fernandez-Carmona, A. Kuzmin, M. Guinchard, A. Slaathaug, C. Hauviller The research leading to these.
B. Caron, G. Balik, L. Brunetti LAViSta Team LAPP-IN2P3-CNRS, Université de Savoie, Annecy, France & SYMME-POLYTECH Annecy-Chambéry, Université de Savoie,
ECES 352 Winter 2007Ch. 8 Feedback – Part 51 Feedback Amplifier Stability *Feedback analysis l Midband gain with feedback l New low and high 3dB frequencies.
Lecture 22: Frequency Response Analysis (Pt II) 1.Conclusion of Bode plot construction 2.Relative stability 3.System identification example ME 431, Lecture.
Frequency Response Analysis and Stability
Frequency Response Analysis
The VIRGO Suspensions Control System Alberto Gennai The VIRGO Collaboration.
Lecture 23: Frequency Response for Design
Sebastian Loeda BEng(Hons) The analysis and design of low-oversampling, continuous-time  converters and the effects of analog circuits on loop stability.
NLC - The Next Linear Collider Project Keeping Nanometer Beams Colliding Vibration Stabilization of the Final Doublet Tom Himel SLAC NLC MAC review October.
ALIGO HSTS Damping Loops Design Comparison J. Kissel, for the SUS and ISC Teams.
ALIGO QUAD "Level 2" Damping Loop Design (Supplemental to LLO aLOG 6949)LLO aLOG 6949 J. Kissel G v21.
ALIGO BSFM “Level 2” Damping Loop Design (Supplemental to LHO aLOG 6392) J. Kissel G v1.
Type-A SAS Local Control Simulation (Current Status)
Control System Analysis and Design by the Frequency Response Method
Way to many People to List
Tuned Mass Damper Investigation for Apache Struts
Seismic Developments at LASTI LIGO-G Z
دکتر حسين بلندي- دکتر سید مجید اسما عیل زاده
Null Space Learning in MIMO Systems
Stability from Nyquist plot
Frequency Response Techniques
Project Goals: The Hardware: The Problem: Results to date:
Radiation pressure induced dynamics in a suspended Fabry-Perot cavity
Measurement of radiation pressure induced dynamics
Frequency Response Techniques
Presentation transcript:

LIGO-G DPage 1 Modal Analysis and Feedback Control of HAM MEPI Oct 16, 2002 Lei Zuo Osamah Rifai Samir Nayfeh

LIGO-G DPage 2 Overview Review of loop transmissions vs. modal data Preliminary look at control –Multiple lightly damped modes close to crossover make control difficult Approaches –Modal control may decrease the relative magnitudes of the flexible modes. –Easiest approach to robust performance: structural damping. –Optimal MIMO Control can improve the performance, but requires a good model

LIGO-G DPage 3 Typical TF from Horizontal Actuator to Geophones 40dB/dec 20dB/dec 18.4Hz 14Hz 16.4Hz 8.6Hz blue 1 red 2 mage 3 green 4 180°-15° Magnitude (dB) Phase

LIGO-G DPage 4 Typical TF from Vertical Actuator to Geophones 40dB/dec 20dB/dec 27.7Hz 29.2Hz 18.5Hz 19.1Hz 14Hz 9.6Hz blue 1 red 2 mage 3 green 4 180°-85° Magnitude (dB) Phase

LIGO-G DPage 5 Observation of this two typical TFs The horizontal-horizontal coupling is very strong, so is vertical-vertical coupling. The vertical -horizontal coupling is very strong at around 3Hz, 19Hz and 28Hz The actuator-sensor pairs seems to be collocated well For control consideration, the critical modes are the two modes around 19Hz, and two modes around 28Hz. (The modes around 14Hz are also critical)

LIGO-G DPage 6 Modal Analysis

LIGO-G DPage 7 Typical Measurement (x) 1.68Hz 2.95Hz 4.4Hz 5.0Hz 6.8Hz 8.4/9.3Hz 9.9/10.9Hz 13.4/13.7Hz 15.7Hz 18.3Hz 18.9Hz 20.38/20.41Hz 27.5/28.7Hz (2.5Hz) 1.3Hz

LIGO-G DPage 8 Typical Measurement (y) 1.68Hz 2.5Hz 4.4Hz (5.0Hz) 6.8Hz 8.4/9.3Hz 9.9/10.9Hz 13.4/13.7Hz 15.7Hz 18.3Hz 18.9Hz 20.38/20.41Hz 27.5/28.7Hz (2.95Hz) (1.3Hz)

LIGO-G DPage 9 Typical Measurement (z) (1.68Hz) 2.95Hz 4.4Hz 5.0Hz 6.8Hz 9.3Hz 9.9/10.9Hz 13.4/13.7Hz 15.7Hz 18.3/18.9Hz 20.38/20.41Hz 27.5/28.7Hz 2.5Hz 1.3Hz 8.4Hz

LIGO-G DPage 10 Critical Modes 15.75Hz, in-plane bending 13.37Hz, in-plane bending + twist13.71Hz, in-plane bending (local) In-plane Beam Bending 18.32Hz, in-plane bending

LIGO-G DPage 11 Critical Modes 18.85Hz, out-of-plane twist Twist

LIGO-G DPage 12 Critical Modes 27.45Hz, tank 28.74Hz, tank Tank Related

LIGO-G DPage 13 Mode Summary Modes at (2.5),3.0, 4.4, 5.0, 6.8, 8.4, and 9.3 Hz are rigid-body modes (compare with Dennis’s modeling?) Modes at 13.4, 13.7, 15.7 Hz, and 18.3 Hz are associated with in-plane bending Mode at 18.9 Hz is related to twist Modes at 27.5 and 28.7 Hz are associated with tank motion Two modes around 20.4 are out-of-plane (vertical) bending Modes at 1.3 and 1.7 Hz seems to be tank motion+frame rigid body (measurements is not so reliable at so low freq) Modes at 9.9, 10.9 are rigid-body plus some bending

LIGO-G DPage 14 Feedback Control of HAM |G(jw)H(jw)| >>1 at low frequency, T(jw)  1/H(jw) |G(jw)H(jw)| <<1 at high frequency, T(jw)  G(jw) G(s), HAM dynamics H(s), sensing and control - + FdV F 1+G(s)H(s) T(s)= G(s)V Fd =

LIGO-G DPage ° - 180° |G(s)| A Control Loop (Concept Design) |H(s)| Phase Margin =75° - |T(s)| Closed Loop 15 reduction 1-3Hz |G(s)H(s)| Loop Gain (The low-frequency characteristics of geophones is not good  Position feedback will be used for <0.5Hz)

LIGO-G DPage 16 F d  V and X 0  X    1 -2/dec -1/dec

LIGO-G DPage 17 Further Consideration The previous concept design is for vertical channels based on the assumption of low plant uncertainties. See the previous control loop again: * Multiple crossing, not robust (unstable!) * PM is 15°, not 75° (add lead? no) See horizontal channels * Multiple crossing, not robust * PM is only 5°

LIGO-G DPage ° - 180° |G(s)| Vertical Loop (Concept Design) |H(s)| Phase Margin =75° =15° - |T(s)| Closed Loop 15 reduction 1-3Hz |G(s)H(s)| Loop Gain Multiple Crossings After Structure Modification (Position feedback will be used for <0.5Hz)

LIGO-G DPage ° - 180° |G(s)| Horizontal Loop (Concept Design) |H(s)| Phase Margin =5° - |T(s)| Closed Loop 15 reduction 1-3Hz |G(s)H(s)| Loop Gain Multiple Crossings After Structure Modification (Position feedback will be used for <0.5Hz)

LIGO-G DPage 20 Suggestion for Feedback Control * Modal Decomposition SISO Control. Questions (SISO): 1) how good is the decomposition? 2) how large are the peaks of flexible modes? Other rigid-body modes from non-perfect decomposition Flexible modes Dominant rigid-body mode  |·||·| 1

LIGO-G DPage 21 Suggestions on Structure Modification (to make control easier) Add constrained layer (viscoelastic) damping to the beam structure (to damp the bending modes) Make the joints stiffer; add some damping to the joints; or add another beam Reduce the coupling between tank and the frame.

LIGO-G DPage 22 Conclusions Multiple lightly damped modes close to crossover make control difficult –Instability –Amplification of disturbances Modal control may decrease their relative magnitudes. Easiest approach to robust performance: structural damping. Optimal MIMO Control can improve the performance, but requires a good model

LIGO-G DPage 23 Other Control Schedules Discussed Osamah: low frequency crossing with high order controller Dave: notch filter Rich, David and Denis: high frequency crossing

LIGO-G DPage 24 Appendix

LIGO-G DPage 25 Typical TF from Horizontal Actuator to Positions Magnitude (dB) Phase

LIGO-G DPage 26 Typical TF from Vertical Actuator to Positions Magnitude (dB) Phase

LIGO-G DPage 27 Out-of-Plane Bending Modes 20.38Hz 20.41Hz Out-of-Plane Beam Bending Related

LIGO-G DPage 28 Mode Shapes 1.3Hz 1.7Hz (low-freq, measurement is not reliable)

LIGO-G DPage 29 Mode Shapes 2.50Hz 2.97Hz

LIGO-G DPage 30 Mode Shapes 4.41Hz 4.99Hz

LIGO-G DPage 31 Mode Shapes 6.86Hz 8.33Hz

LIGO-G DPage 32 Mode Shapes 9.25Hz

LIGO-G DPage 33 Mode Shapes 10.9Hz 9.82Hz