CARE / ELAN / EUROTeV 20071 Active stabilization of a mechanical structure Laurent BRUNETTI LAViSta Team LAPP-IN2P3-CNRS,

Slides:



Advertisements
Similar presentations
Chapter3 Pulse-Echo Ultrasound Instrumentation
Advertisements

Chapter 4: Basic Properties of Feedback
Passive isolation: Pre-isolation for FF quads A. Gaddi, H. Gerwig, A. Hervé, N. Siegrist, F. Ramos.
Lorentz force detuning measurements on the CEA cavity
CLIC stabilisation contribution A.Jeremie, B.Caron, A.Badel, R.LeBreton, J.Lottin, G.Balik, J.P.Baud, L.Brunetti, G.Deleglise, S.Vilalte.
1 LAViSta Laboratories in Annecy working on Vibration and Stabilisation Impact of random and determinist acoustic noise on vibrations at high frequencies.
1 Unité mixte de recherche CNRS-IN2P3 Université Paris-Sud Orsay cedex Tél. : Fax :
SIMPLIFIED MODELS OF ILD AND SID DETECTORS: SIMULATIONS AND SCALED TEST ULB: Christophe Collette, David Tschilumba, Lionel SLAC: Marco.
Takanori Sekiguchi Italy-Japan Workshop (19 April, 2013) Inverted Pendulum Control for KAGRA Seismic Attenuation System 1 D2, Institute for Cosmic Ray.
CHE 185 – PROCESS CONTROL AND DYNAMICS
CHE 185 – PROCESS CONTROL AND DYNAMICS
CHE 185 – PROCESS CONTROL AND DYNAMICS
Slide# Ketter Hall, North Campus, Buffalo, NY Fax: Tel: x 2400 Control of Structural Vibrations.
280 SYSTEM IDENTIFICATION The System Identification Problem is to estimate a model of a system based on input-output data. Basic Configuration continuous.
The Mechatronics Design Lab Course at the University of Calgary Presented June 2, 2003.
Benoit BOLZON Nanobeam 2005 – Kyoto Active mechanical stabilisation LAViSta Laboratories in Annecy working on Vibration Stabilisation Catherine ADLOFF.
Stabilization of the FF quads A.Jeremie B.Bolzon, L.Brunetti, G.Deleglise, N.Geffroy A.Badel, B.Caron, R.Lebreton, J.Lottin Together with colleagues from.
QD0 stabilisation update (since last update in MDI) A.Jeremie A.Badel, B.Caron, R.LeBreton, J.Lottin, J.Allibe, G.Balik, J.P.Baud, L.Brunetti, G.Deleglise.
Luminosity Stability and Stabilisation Hardware D. Schulte for the CLIC team Special thanks to J. Pfingstner and J. Snuverink 1CLIC-ACE, February 2nd,
Eurotev Feedback Loop for the mechanical Stabilisation Jacques Lottin* Laurent Brunetti*
B. Caron, G. Balik, L. Brunetti LAViSta Team LAPP-IN2P3-CNRS, Université de Savoie, Annecy, France & SYMME-POLYTECH Annecy-Chambéry, Université de Savoie,
1 LAViSta Laboratories in Annecy working on Vibration and Stabilisation Catherine ADLOFF Andrea JEREMIE Jacques LOTTIN Benoît BOLZON Yannis KARYOTAKIS.
1 ATF2 project: Investigation on the honeycomb table vibrations Benoit BOLZON 33rd ATF2 meeting, 24th January 2007 Laboratories in Annecy working on Vibration.
Vibrationdata 1 Unit 19 Digital Filtering (plus some seismology)
Vibration measurements on the final doublets and the Shintake Monitor Benoît BOLZON7th ATF2 project meeting, 16/12/08.
Concepts for Combining Different Sensors for CLIC Final Focus Stabilisation David Urner Armin Reichold.
Effect of Mutual Coupling on the Performance of Uniformly and Non-
Installation of FD in September A.Jeremie, B.Bolzon, N.Geffroy, G.Gaillard, J.P.Baud, F.Peltier With the help of KEK, SLAC, KNU and CERN colleagues For.
IN2P3 Les deux infinis G. Balik, B. Caron, L. Brunetti (LAViSta Team) LAPP-IN2P3-CNRS, Université de Savoie, Annecy, France & SYMME-POLYTECH Annecy-Chambéry,
QD0 stabilization L. Brunetti 1, N. Allemandou 1, J.-P. Baud 1, G. Balik 1, G. Deleglise 1, A. Jeremie 1, S. Vilalte 1 B. Caron 2, C. Hernandez 2, (LAViSta.
1 LAPP in ATF2 Extraced from ANR bid A.Jeremie. 2 LAPP in ATF2 Current activities related to accelerators: The LAPP-Annecy team is currently developing.
CLIC QD0 Stabilization J. Allibe 1, L. Brunetti 1, J.-P. Baud 1, G. Balik 1, G. Deleglise 1, A. Jeremie 1, S. Vilalte 1 B. Caron 2,C.Hernandez 2 1 : LAPP-IN2P3-CNRS,
CLIC MDI stabilization update A.Jeremie G.Balik, B.Bolzon, L.Brunetti, G.Deleglise A.Badel, B.Caron, R.Lebreton, J.Lottin Together with colleagues from.
CLIC MDI Working Group Vibration attenuation via passive pre- isolation of the FF quads A. Gaddi, H. Gerwig, A. Hervé, N. Siegrist, F. Ramos.
Progress in identification of damping: Energy-based method with incomplete and noisy data Marco Prandina University of Liverpool.
Minimizing the Resonant Frequency of MGAS Springs for Seismic Attenuation System in Low Frequency Gravitational Waves Interferometers Maddalena Mantovani,
July 5, 2007 C. HAUVILLER CLIC stabilization Beam line and final focus.
CARE / ELAN / EUROTeV Feedback Loop on a large scale quadrupole prototype Laurent Brunetti* Jacques Lottin**
Control systems KON-C2004 Mechatronics Basics Tapio Lantela, Nov 5th, 2015.
1 FP7 LED Potential program to develop inertial sensors Explore potential to achieve 0.1nm stability scale for the FD above a few Herz A.Jeremie, C.Hauviller.
Lecture 25: Implementation Complicating factors Control design without a model Implementation of control algorithms ME 431, Lecture 25.
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,
Adaptive Control Loops for Advanced LIGO
1 ATF2 Project Meeting December 2006 Ground Stabilisation with the CERN STACIS 2000 Stable Active Control Isolation System LAViSta Laboratories in.
Main beam Quad Stabilisation: Status of the stabilisation test program at CERN CLIC-stabilization day S. Janssens Contribution to slides by:
Passive isolation: Pre-isolation for FF quads A. Gaddi, H. Gerwig, A. Hervé, N. Siegrist, F. Ramos.
STABILISATION AND PRECISION POINTING QUADRUPOLE MAGNETS IN THE COMPACT LINEAR COLLIDER S. Janssens, P. Fernandez Carmona, K. Artoos, C. Collette, M. Guinchard.
Superconducting final doublet Support A.Jeremie. SC magnet steps Motivation: have an active stabilisation as planned in ILC and CLIC => need to evaluate.
DEPARTMENT OF MECHANICAL TECHNOLOGY VI -SEMESTER AUTOMATIC CONTROL 1 CHAPTER NO.6 State space representation of Continuous Time systems 1 Teaching Innovation.
CERN, 27-Mar EuCARD NCLinac Task /3/2009.
State-Space Recursive Least Squares with Adaptive Memory College of Electrical & Mechanical Engineering National University of Sciences & Technology (NUST)
ATF2: final doublet support Andrea JEREMIE B.Bolzon, N.Geffroy, G.Gaillard, J.P.Baud, F.Peltier With constant interaction with colleagues from KEK, SLAC.
NLC - The Next Linear Collider Project Keeping Nanometer Beams Colliding Vibration Stabilization of the Final Doublet Tom Himel SLAC NLC MAC review October.
QD0 stabilisation in CLIC CDR A.Jeremie with LAViSta team.
Vibration measurements with and without Monalisa 15/07/09 Benoît BOLZON (LAPP) David Urner (Oxford) Paul Coe (Oxford) 1 Benoît BOLZON.
FF Stabilisation A.Jeremie (Summary of things learned and work done at LAPP, CERN, SYMME, Oxford, SLAC)
QD0 Stabilisation L. Brunetti 1, J. Allibe 1, J.-P. Baud 1, G. Balik 1, G. Deleglise 1, A. Jeremie 1, S. Vilalte 1 B. Caron 2, A. Badel 2, R. Le Breton.
CARE05 – November Status report on active stabilisation of a linear collider final focus quadrupole mock-up J. Lottin, ESIA
Intelligent Control Grant Agreement No LLP UK-LEONARDO-LMP Project acronym: CLEM Project title: Cloud services for E-Learning in Mechatronics.
Vibration issues at Linear Colliders:
Chapter 1: Overview of Control
OSE801 Engineering System Identification Spring 2010
Active isolation Target : a low cost dedicated table
3: ISI ASCR, Brno University of Technology, Brno, Czech Republic
Laboratories in Annecy working on Vibration Stabilization
FP7 LED A.Jeremie, L.Brunetti, N.Geffroy.
Superattenuator for LF and HF interferometers
Assessment of Base-isolated CAP1400 Nuclear Island Design
Towards a ground motion orbit feed-forward at ATF2
Presentation transcript:

CARE / ELAN / EUROTeV Active stabilization of a mechanical structure Laurent BRUNETTI LAViSta Team LAPP-IN2P3-CNRS, Université de Savoie, Annecy, France & SYMME-POLYTECH’SAVOIE, Annecy, France

CARE / ELAN / EUROTeV Overview 1. Introduction and our approach of the stabilization problem : - Problem of structure stabilization and our point of view - Active control at a nanometer scale at given frequencies - Limitations of this method 2. The last tested algorithm : command with local internal model - Brief description - Numerical approach to increase the tests possibilities - Results in simulation mode - Results at the nanometer scale with the prototype 3.A beginning of active isolation study : - Previous study and the interest in exploring this aspect - Current work 4. Conclusion and perspectives

CARE / ELAN / EUROTeV e-e+e- The problem of the stabilization The sources of the structure motion : Direct effects : Acoustic disturbances The different required approaches of this problem : Final focus Introduction Indirect effects : Ground motion (seismic + cultural noise)  Direct effects : - excite particularly the resonant modes of the structure  Indirect effects : - create a vertical displacement of the clamping - excite particularly the vertical flexion mode of the structure  Active compensation : - maintain the structure in a straight horizontal position along its axe  Active and passive isolation : - obtain a null absolute displacement of the clamping, so of the entire system.

CARE / ELAN / EUROTeV Introduction Example of spectral analysis of different disturbance sources Acoustic disturbance : Amplified by the structure itself : the eigenfrequencies Ground motion : Seismic motion Cultural noise A pink noise on a large bandwidth

CARE / ELAN / EUROTeV What is the feedback loop based on? Introduction Different approaches of the problem 1 - A complete model of the structure : too complex 2 - A knowledge of the structure at strategic points : the initially developed algorithm An example of displacement of a mechanical structure : f0f0 f1f1 fifi A complete model of the process A knowledge of the process at strategic points

CARE / ELAN / EUROTeV The first developed algorithm The originality : Active compensation The different components : Signal processing (transposition in a new basis) State observer State feedback Rebuilding of the strength y c (w i ) y s (w i ) f c (w i ) f s (w i ) y f f c (w i ) f s (w i ) Structure to be stabilised SensorActuator Filtering (at one frequency) y(w i ) Spectral analysis Not based on a model of the system (classical algorithm), but only on a few characteristics of the system, computed in open loop for each selected frequency : - The gain and the phases differences between output / input. - The setting time.

CARE / ELAN / EUROTeV The prototype Active compensation 2.5 m long The large prototype and its instrumentation : Actuators used for the active control of vibration :  Force = 19.3 N  Maximal displacement = 27,8 μm  Resolution = 0,28 nm - A stacking of PZT patches -

CARE / ELAN / EUROTeV The components of the prototype Sensors are used to measure the structure motion (non magnetic) : Real time solution : a rapid prototyping of Mathworks (XPC Target) Active compensation Analogical digital cards : PCI 6052E (NI) Fast cardLow noise card

CARE / ELAN / EUROTeV Results with the first developed algorithm The first results at the nanometer scale :  Active compensation is efficient with this initial algorithm for narrow peaks.  For eigenfrequencies, the need of controlling a larger bandwidth.  Example of active compensation of an unknown frequency disturbance, excited by the natural environment (motion of the ground + acoustic noise).  Possibilities to increase the number of rejected disturbances. Active compensation

CARE / ELAN / EUROTeV Another approach of the problem Active compensation Test an intermediary solution : to control a larger bandwidth 3 - A local model of the structure : for the disturbances amplified by eigenfrequencies. 1 - A complete model of the structure : too complex 2 - A knowledge of the structure at strategic points : the initially developed algorithm f0f0 f1f1 fifi A complete model of the process A knowledge of the process at strategic points A local model of the process

CARE / ELAN / EUROTeV The basic principle of a command with internal model : Command with internal model Active control CIM  The command u(s) : - is applied simultaneously to the process and to the model. - is not computed in function of the output y(s) but of the difference between the measured output and the output of the model.  The output y(s) is compared to the output of the model : ε(s)=[P(s)-M(s)].u(s)+d(s)withu(s)=[e(s)-ε(s)].C(s)  The controller C(s) is built in function of the model. Corrector C(s) Model M(s) Process P(s) u(s) + + disturbances d(s) y(s) ε(s) Setpoint e(t) y e (s)

CARE / ELAN / EUROTeV The basic principle of a command with internal model : Command with internal model Active control CIM  The transfer function of CIM in closed loop is : Corrector C(s) Model M(s) Process P(s) u(s) + + disturbances d(s) y(s) ε(s) Setpoint e(t) y e (s)  To cancel the disturbance : C(s) = M(s) -1  Controller = inverse (Model)  To follow the setpoint : M(s) ~ P(s)  Model ~ Process

CARE / ELAN / EUROTeV Corrector C(s) Local model M(s) Process P(s) u(s) + + disturbances d(s) y(s) ε(s) Setpoint e(t) The used adaptation for our problem : Command with internal model Active control CIM  The model M(s) is an elementary model, which corresponds locally to the process, so it is defined in function of a basic knowledge of the process : - The amplification and the phase at the selected resonant frequency. - The damping of the selected resonant mode (hammer test, in function of the gain)  The filter F(s) selects the bandwidth of the algorithm.  The requirements of this algorithm are a bit more complex but still basic, so realistic !!  There are as many algorithms in parallel as there are eigenfrequencies to stabilize. y e (s) Filter F(s)

CARE / ELAN / EUROTeV A finite element model of the structure : Tests in simulation Active control CIM Dynamics equation :  M : Mass matrix  C : damping matrix  K : stiffness matrix  Require an updating to be as representative as possible to the real setup The interest of the simulation :  To adjust the feedback loop  To increase the tests possibilities (multiple configuration for sensors, actuators…)  To analyse the behaviour of the entire beam  A prediction of the mechanical structure response Ex : force (actuator) applied to a point

CARE / ELAN / EUROTeV FE Model Creation SAMCEF M : mass matrix C : damping matrix K : stiffness matrix State-Space Model Creation MATLAB x : state vector u : input vector y : output vector Simulink State-Space Model Use in : accel / force perturb. + force actuator out : accel / velocity / displacement Integration of a finite element in a feedback loop : Tests in simulation Active control CIM

CARE / ELAN / EUROTeV Tests in simulation Active control CIM Integration of the finite element model in the feedback loop : Example of result :

CARE / ELAN / EUROTeV Test at an nanometer scale with natural disturbance sources : Tests with the large prototype Active control CIM Sensor : velocity sensor at the end of the beam. Actuator : actuator in flexion mode as close as possible on the clamping

CARE / ELAN / EUROTeV Results : Power spectral density Tests with the large prototype Active control CIM

CARE / ELAN / EUROTeV Results : integrated displacement RMS Tests with the large prototype Active control CIM

CARE / ELAN / EUROTeV Results : integrated displacement RMS Tests with the large prototype Active control CIM

CARE / ELAN / EUROTeV Results : Power spectral density (with active table ON) Tests with the large prototype Active control CIM

CARE / ELAN / EUROTeV Results : integrated displacement RMS (with active table ON) Tests with the large prototype Active control CIM 1 nm Actuator electronic noise at 50 Hz

CARE / ELAN / EUROTeV Current state : Tests with the large prototype Active control CIM  This method is efficient and easily adaptive to a mechanical structure  Obtain these last results but in a critical configuration (for example when the motion of the beam is without rejection about 30 to 100 nm)  Obtain these results all along the beam  Minimize the influence of a bandwidth rejection on the neighbour frequencies.  Finish the robustness tests.  Parallelize a second real time setup for increasing the number of rejected disturbances (with mixed types of algorithms), in order to obtain an optimal RMS.  Combine with active isolation. Current and future works :

CARE / ELAN / EUROTeV The industrial solution Active isolation Test of industrial solutions : the TMC table of CERN.  Efficient but partially a “black box”… Composed of a passive bloc, placed on 4 active feet (STACIS). Principle and all characteristics are known but the process is unknown.

CARE / ELAN / EUROTeV Active isolation  Test of active isolation on a small mock-up…  Passive isolation : attenuates all the high frequency disturbances but amplifies the low frequency disturbances (like a resonant filter).  Active isolation : attenuates the disturbance amplified by the passive isolation (low frequencies disturbances). (Thesis of S. Redealli) In the case of a possible partnership, we have no competence about active isolation. In the case of the development of a low cost table (this one is very expensive), we have no information about the mechanism (mainly the feedback loop). STACIS foot : Reasons of this study and the STACIS feet

CARE / ELAN / EUROTeV Association of active and passive isolation :  Not heavy enough to use industrial products, but it is possible with a larger prototype. The small and elementary mock-up Active isolation The passive layer : Require active isolation Δf Passive isolation is efficient Resonant frequency of the rubber

CARE / ELAN / EUROTeV Algorithm : test with the LQG command (Linear Quadratic Gaussian) The active part Active isolation  The Model is definable, so a classical algorithm based on a model is appropriate.  This type of algorithm is adapted for noisy system, so for the seismic domain. Simulation under Matlab - Simulink in state space representation : - Test of a mass - spring system excited by a measured sequence of the ground motion Test in real time with the small built mock-up :  Depending on the quality of the results, possible transposition to support the large mock-up with industrial rubber, in order to have a complete solution with the active compensation.  Future works : expected results at the next meeting!!

CARE / ELAN / EUROTeV Hardware : Conclusions  Acquisition chain able to measure at a nanometer scale  Actuators to create nanometer displacements  A real time solution to run automatics algorithm Control :  2 types of algorithms for active compensation  A beginning of study for active isolation Future prospects :  The purpose now is to obtain the best possible stabilization all along the elementary mechanical structure (lower or equal to the imposed tolerance)  We have succeeded in stabilizing an elementary structure at a nanometer scale with a natural environment.

CARE / ELAN / EUROTeV ANNEXES

CARE / ELAN / EUROTeV  Amplification in open loop.  Difference of phase in open loop.  Setting time.  Determinate a model which corresponds to the process for the selected bandwidth with the same : - Amplification in open loop. - Difference of phase in open loop. - Damping of the selected eigenfrequency.  Build a corrector from this model, which is stable, meaning respects the rules of automatic. State spaceCommand with internal model Active control CIM Similarities of tuning between the initial algorithm (state space for punctual disturbances) and this one (CIM for large peaks) : To determinate the damping values, there are different methods : - Theoretical : modelling… - Experimental : hammer test, in function of the amplification…  The requirements of this algorithm are a bit more complex but still basic, so realistic !!

CARE / ELAN / EUROTeV Results : transfer function between the displacement at the clamping and at the end of the beam : Tests with the large prototype Active control CIM

CARE / ELAN / EUROTeV Sensors noise measurement at LAPP Sensors noise estimation (Corrected difference calculation):  Two sensors of the same model put side-by-side (2 SP500 sensors) Environmental conditions: 1.Very low ground motion (coherence as low as possible: best estimation) 2.Low-frequency noise: No fast temperature and pressure change in time 1. Sensors on the CLIC active table / Measurements done the night / Shutdown of all computers / Acquisition system outside the room 2. Ventilation cut / Doors closed: 10 hours before measurements