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CSEM Scientific and Technical Report 2008

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European Large Telescope M5 Field Stabilization Unit: Mirror-control<br />

O. Chételat, E. Onillon, Y. Welte<br />

The control design <strong>and</strong> performance analysis of the M5, one of the mirrors of the "Adaptative European Extremely Large Telescope", is presented<br />

in this paper as a companion to another article of this report entitled "European Large Telescope M5 Field Stabilisation Unit: Opto-mechatronics".<br />

Figure 1 shows the M5 mirror attached to its base by three<br />

actuators <strong>and</strong> a membrane in the center. The actuators are<br />

made of a piezo stack with its elongation being amplified by a<br />

parallelogram flexure.<br />

Figure 1: M5 mirror <strong>and</strong> detail of one of the three piezo actuators<br />

The M5s dedicated task is to reject – in a tip-tilt motion – the<br />

disturbances due to the wind load on the telescope structure<br />

<strong>and</strong> to the atmosphere. Figure 2 shows the power spectrum of<br />

the total disturbance for one axis.<br />

PSD (arcsec 2 /Hz)<br />

Figure 2: Power spectrum of wind <strong>and</strong> atmospheric disturbance nφ<br />

Figure 3 depicts the dynamic modeling of the M5 in closed<br />

loop. The optics of the telescope sees the two tip-tilt angles<br />

described by the vector φ. The difference between these<br />

angles <strong>and</strong> the ones of the mirror is due to the disturbance nφ.<br />

0<br />

M5 mirror<br />

10 10<br />

10 0<br />

10 -10<br />

10 -2<br />

10 -20<br />

K E<br />

z=0<br />

1-z -1 s -1<br />

K o<br />

10 -1<br />

M * T<br />

M *<br />

10 0<br />

10 1<br />

frequency (Hz)<br />

actuator<br />

piezo<br />

Figure 3: Dynamic modeling of M5 in closed loop<br />

u<br />

n u<br />

K i<br />

1/R<br />

na s2 a<br />

n x<br />

F<br />

1/Cs ke The mirror angles are linearly calculated from the elongation<br />

of the three actuators (vector x) by a matrix M, because the<br />

angles are assumed small. The mechanical transfer function<br />

G between the piezo force F <strong>and</strong> the actuator <strong>and</strong> piezo<br />

elongations x <strong>and</strong> p (respectively) is obtained by a detailed<br />

FEM modal frequency response analysis as shown in Figure 4.<br />

The electro-mechanical action of the piezo transducers is<br />

modeled taking into account the force constant ke, the piezo<br />

capacitance C <strong>and</strong> the supply line resistance R (the Laplace<br />

variable is denoted by s). It is assumed that the actuator<br />

elongation x as well as the acceleration a of the piezo<br />

sk e<br />

10 2<br />

G<br />

x<br />

x<br />

p<br />

M<br />

p<br />

10 3<br />

nφ φ<br />

elongation are measured. The optical tip-tilt angles are also<br />

measured with a wave-front sensor modeled as (1−z −1 )/s,<br />

where z = e sT (with T the sample time).<br />

Three control loops are considered. The inner-loop based on<br />

the acceleration a is used to "damp" the system in a robust<br />

way, i.e., based on the passivity (emulation of a viscous<br />

friction thanks to the velocity feedback obtained by integration<br />

of a by Ki <strong>and</strong> acting on the piezo voltage u). At 1 kHz sample<br />

frequency, the middle loop controls the mechanism in the<br />

angles-piston domain using the controller Ko as well as the<br />

transformation matrices M* (similar to the matrix M, but<br />

including the piston) <strong>and</strong> its transposed M* T . Finally, the outer<br />

loop is used with the controller KE at a lower sample frequency<br />

(100 Hz) imposed by the technology of the wave-front sensor.<br />

x 2 / F 2 (m/N)<br />

10 -6<br />

10 -8<br />

10 -10<br />

10 0<br />

10 -12<br />

10 1<br />

frequency (Hz)<br />

Figure 4: Frequency response representing one input of the<br />

mechanical transfer function matrix G obtained by finite-element<br />

computation.<br />

The dynamic model of Figure 3 optimizes the controllers of the<br />

three loops <strong>and</strong> computes the noise in closed loop. Table 1<br />

shows in the first column the maximum noise requirements, in<br />

the second column the residual noise from the rejected wind<br />

<strong>and</strong> atmospheric disturbances, <strong>and</strong> in the three last columns,<br />

the noise that would be obtained if 10-bit quantizing for the<br />

voltage u, the acceleration a, <strong>and</strong> the position x, respectively<br />

were assumed.<br />

Table 1: Computed performances of M5 (all units in milli-arcsec)<br />

Requirements output volt. u acc. a pos. x<br />

dist. nφ 10 bits 10 bits 10 bits<br />

< 70 rms (0…∞Hz) 27.4 1.6 0.001 0.6<br />

< 4 rms (9…∞Hz) 0.67 1.6 0.001 0.6<br />

< 8 max (9…∞Hz) 3 7 0.005 2.4<br />

Table 2 lists the final specifications allowing the M5 to be<br />

within the requirements. These specifications are derived from<br />

the control design for the range, resolution, <strong>and</strong> analogue<br />

noise of the voltage u, the acceleration a, <strong>and</strong> the position x.<br />

Table 2: Specifications of electronics derived from control design<br />

Specifications voltage u acceler. a position x<br />

Full range (with margin) 1000 V 2 mm/s 2 0.6 mm<br />

ADC/DAC resolution ≥ 13 bits ≥ 2 bits ≥ 11 bits<br />

Analogue noise (rms) 69 mV 0.24 mm/s 2 88 nm<br />

Thanks to the methodology described in this paper, it has<br />

been possible to specify an electronics that fulfils the<br />

customer requirements.<br />

10 2<br />

91

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