PSN-L Email List Message

Subject: Re: AD7142 ? Capacitative sensors
From: ChrisAtUpw@.......
Date: Thu, 13 Apr 2006 20:30:27 EDT


In a message dated 13/04/2006, barry_lotz@............. writes:

Hi Brett
  STM wrote as a solution to LVDTs "The common solution is to use a =20
capacitive bridge transducer, where a moving vane moves between two fixed  p=
lates that=20
form a capacitive bridge that is unbalanced by the movement of the  vane.=20
With proper geometry, these can be very sensitive and linear over a  range o=
f=20
several hundred microns.

Hi Barry,
=20
    The capacitance in pF =3D 0.0885xAxK / d, where A is  the plate area in=20=
sq=20
cm, K is the dielectric constant and d is the plate  separation in cm.=20
    With proper design, sensors can be linear over +/-5  mm or more. It=20
depends on what you need. It may be difficult to get the noise  below 1 ppm=20=
x range=20
for 10 Hz bandwidth, but it can be done.

However, they are difficult to construct and have a working gap of less  tha=
n=20
a millimetre, and are prone to off axis sensitivity.=20

    This is largely incorrect for amateur applications.  If you demand 1nm=20
resolution or better, you do need special materials and  construction -> Sil=
ver=20
coated Invar / Platinum coated Quartz electrodes.=20
=20
    There are three basic types of capacitor sensor.  You can have a pair of=
=20
parallel plates excited by sine or square waves with a  central sensor plate=
=20
which moves perpendicular to the plane. This needs  voltage detection to be=20
highly linear and has a range limited by  the separation of the outer plates=
 -=20
likely to be quite limited. If you use  charge sensing, the linear range is=20
reduced to maybe 1/4. You are likely to  have to bore holes in the plates to=
 allow=20
adequate airflow as they move.
    You can use two pairs of parallel plates with a  central sensor plate=20
moving parallel to the plane - a split stator  variable capacitor. The excit=
ation=20
is applied between the pairs of plates on  opposite sides of the sensor=20
plate. Charge detection is usually used with an  electrical connection to ce=
ntral=20
plate. The sensor range depends on  the width of the moving plate, which is=20
half the overall stator width.  There is no air flow problem with plate move=
ment.
    You can use basically parallel circuit board plates  with a pair of=20
excitation strips on one side, a cross coupled square /  rectangular sense a=
rray on=20
the other and a plate with vertical 'shadow strips'  moving parallel in=20
between. It is easy to make these out of double sided  glass circuit board.=20=
The=20
central shadow plate does not need to be earthed.  Only the fixed plates nee=
d to=20
be wired up, which is a considerable  advantage. The maximum movement is hal=
f=20
the square 'cell size'. Again  this can be quite large. See Randall Peters'=20
SDC sensor at _http://physics.mercer.edu/petepag/sens.htm_=20
(http://physics.mercer.edu/petepag/sens.htm)  Charge  detection is usually u=
sed. An array of=20
coupled cells can be used to increase the  sensitivity. It is an advantage t=
o make=20
the shadow plate out of etched double  sided glass board. The 'electrical=20
thickness' is the actual thickness divided by  the dielectric constant. Havi=
ng all=20
three boards made from the same material  greatly reduces any thermal drift.=
=20
There is no air flow problem with plate  movement.

They usually operate at relatively high frequencies, from khz to mhz,  which=
=20
complicates design and implementation problems"=20

    Operating at 10 to 50 k Hz is just fine. You can  use digital to sine=20
weighted step down counters which give very good sine waves  - see=20
_http://www.eas.slu.edu/People/STMorrissey/index.html_=20
(http://www.eas.slu.edu/People/STMorrissey/index.html)    Alternatively, you=
 can use a LTC1043 quad chopper switch=20
/ oscillator with  either sine or square waves. Using sine waves allows you=20=
to=20
get a higher  S/N ratio. XR8038 & especially XR2206 function generators can=20
give quite a  good performance, as can a FET stabilised Wein Bridge oscillat=
or=20
- see _http://www.keckec.com/seismo/_ (http://www.keckec.com/seismo/) . Two=20=
=20
stages of RC bandpass filter are used in=20
_http://psn.quake.net/info/bb13OperManual.pdf_ (http://psn.quake.net/info/bb=
13OperManual.pdf)  starting  with the=20
square wave from a quartz oscillator. For low drift, avoid  resonant circuit=
s=20
and diode rectification.

It looks like the AD device would solve some of these  concerns.=20

    The concerns seem to be largely illusory in  practice.
=20
=20
In a message dated 13/04/2006 14:48:47 GMT Daylight Time, =20
Brett3kg@............. writes:=20

Biggest  VRDT problem seems to be its low drive frequency. In a feedback =20
design the large demod filters are prime contributors to loop oscillation =20
problems.
    So reduce the filtration and apply a DC + pulsed  feedback? Use another=20
method?
    The feedback phase delay is only a problem if you  do it this way!

>I'm  not sure about the noise. Does the VBB measure displacements in the 1=20=
=20
>=B1 nm range?

With the sensor plates above, 1LSB=3D0.08nm.   But I think noise is what=20
determines the useful resolution.  However  0.3nm / sqrt-Hz and 2.1nm RMS at=
=20
50 SPS isn't too shabby.  It would  be interesting to assume a seismic-mass=20
system and model how this would  compare with commercial instruments and=20
earth-noise models.  I'm  betting it won't look so bad.
    Have you measured your environmental noise level?  Is 2.1 nm a realistic=
=20
target? The amplitude of the 6 second ocean microseisms  may be from 500 to=20
15,000 nm!

=20
He  then goes on to describe the VRDT. I suppose for the VBB sensor this=20
would  greatly simplify the electronic design if one can deal with small sen=
sor =20
gaps. I'm not sure about the noise. Does the VBB measure displacements in  t=
he=20
1 =B1 nm range?   --- Just thinking out loud. I think it greatly  depends on=
=20
what type of sensing one wants to do local, regional or  teleseismic.

      Amateur seismometers are usually  limited by either microseisms or by=20
environmental noise - we can't usually  choose a quiet remote site. I manage=
d=20
to reduce the noise of my LVDT to about 7  nm for a 6 mm range at 10 Hz, but=
 my=20
environmental noise is much greater  than this.=20
=20


It would  be great to be able to use this with feedback.  No question that=20
you  could use it for integral feedback, which mainly works below the low =20
frequency roll off (say, below 0.011 Hz).  You could make an awesome =20
integrator by digital summing, then feed back with a D/A.  Mid  frequency=20
range (derivative feedback) may not be practical.  Although  you could keep=20
your beam well centred with integral feedback, without  derivative feedback=20
at higher frequencies, you're limited by the +/- 1.0mm  (+/- 0.5 mm max, for=
=20
linearity) sensor gap.  I'm suspecting that  clipping levels in the=20
mid-frequency range are going to be the biggest  limitation.




So, we may need some 'lateral thinking'  here! There are 'problems that you=20
do not need to have' - like:-
=20
    The velocity feedback damping does not need to be  generated that way!
=20
    Neither do we need to use that troublesome design  of capacitative senso=
r!
=20
 ***   You can use JUST position +  integral current / coil feedback if you=20
ALSO have a quad magnet +  Cu plate for the velocity damping! Trying to prov=
ide=20
velocity damping by  differentiation and coil feedback is likely to very=20
significantly increase the  overall circuit noise!  ***
=20
    Regards,
=20
    Chris Chapman






In a message dated 13/04/2006, barry_lotz@............. writes:
<= FONT=20 style=3D"BACKGROUND-COLOR: transparent" face=3DArial color=3D#000000 size= =3D2>
Hi Brett
  STM wrote as a solution to LVDTs "The common solution is to us= e a=20 capacitive bridge transducer, where a moving vane moves between two fixed=20 plates that form a capacitive bridge that is unbalanced by the movement of= the=20 vane. With proper geometry, these can be very sensitive and linear over a=20 range of several hundred microns.
Hi Barry,
 
    The capacitance in pF =3D 0.0885xAxK / d, where= A is=20 the plate area in sq cm, K is the dielectric constant and d is the plate=20 separation in cm.
    With proper design, sensors can be linear over=20= +/-5=20 mm or more. It depends on what you need. It may be difficult to get the nois= e=20 below 1 ppm x range for 10 Hz bandwidth, but it can be done.
However, they are difficult to construct and have a working gap o= f less=20 than a millimetre, and are prone to off axis sensitivity.=20
    This is largely incorrect for amateur applicati= ons.=20 If you demand 1nm resolution or better, you do need special materials and=20 construction -> Silver coated Invar / Platinum coated Quartz electrodes.=20
 
    There are three basic types of capacitor sensor= ..=20 You can have a pair of parallel plates excited by sine or square waves with=20= a=20 central sensor plate which moves perpendicular to the plane. This nee= ds=20 voltage detection to be highly linear and has a range limited by=20 the separation of the outer plates - likely to be quite limited. If you= use=20 charge sensing, the linear range is reduced to maybe 1/4. You are likel= y to=20 have to bore holes in the plates to allow adequate airflow as they move.
    You can use two pairs of parallel plates with a= =20 central sensor plate moving parallel to the plane - a split stator=20 variable capacitor. The excitation is applied between the pairs of plates on= =20 opposite sides of the sensor plate. Charge detection is usually used with an= =20 electrical connection to central plate. The sensor range depends on=20 the width of the moving plate, which is half the overall stator wi= dth.=20 There is no air flow problem with plate movement.
    You can use basically parallel circuit board pl= ates=20 with a pair of excitation strips on one side, a cross coupled square /=20 rectangular sense array on the other and a plate with vertical 'shadow strip= s'=20 moving parallel in between. It is easy to make these out of double si= ded=20 glass circuit board. The central shadow plate does not need to be earth= ed.=20 Only the fixed plates need to be wired up, which is a considerable=20 advantage. The maximum movement is half the square 'cell size'. Aga= in=20 this can be quite large. See Randall Peters' SDC sensor at http://physics.mercer.ed= u/petepag/sens.htm Charge=20 detection is usually used. An array of coupled cells can be used to increase= the=20 sensitivity. It is an advantage to make the shadow plate out of etched doubl= e=20 sided glass board. The 'electrical thickness' is the actual thickness divide= d by=20 the dielectric constant. Having all three boards made from the same material= =20 greatly reduces any thermal drift. There is no air flow problem with plate=20 movement.
They usually operate at relatively high frequencies, from khz to=20= mhz,=20 which complicates design and implementation problems"
    Operating at 10 to 50 k Hz is just fine. You ca= n=20 use digital to sine weighted step down counters which give very good sine wa= ves=20 - see http://www.eas= ..slu.edu/People/STMorrissey/index.html =20 Alternatively, you can use a LTC1043 quad chopper switch / oscillator w= ith=20 either sine or square waves. Using sine waves allows you to get a highe= r=20 S/N ratio. XR8038 & especially XR2206 function generators can give quite= a=20 good performance, as can a FET stabilised Wein Bridge oscillator - see http://www.keckec.com/seismo/. Tw= o=20 stages of RC bandpass filter are used in http://psn.quake.net/i= nfo/bb13OperManual.pdf starting=20 with the square wave from a quartz oscillator. For low drift, avoid=20 resonant circuits and diode rectification.
It looks like the AD device would solve some of these=20 concerns. 
    The concerns seem to be largely illusory in=20 practice.
 
 
In a message dated 13/04/2006 14:48:47 GMT Daylight Time,=20 Brett3kg@............. writes:
<= FONT=20 style=3D"BACKGROUND-COLOR: transparent" face=3DArial color=3D#000000 size= =3D2>Biggest=20 VRDT problem seems to be its low drive frequency. In a feedback=20
design the large demod filters are prime contributors to loop oscillat= ion=20 problems.
    So reduce the filtration and apply a DC + pulse= d=20 feedback? Use another method?
    The feedback phase delay is only a problem if y= ou=20 do it this way!
<= FONT=20 style=3D"BACKGROUND-COLOR: transparent" face=3DArial color=3D#000000 size= =3D2>>I'm=20 not sure about the noise. Does the VBB measure displacements in the 1=20
>=B1 nm range?

With the sensor plates above, 1LSB=3D0.08nm.&= nbsp;=20 But I think noise is what
determines the useful resolution.  Howe= ver=20 0.3nm / sqrt-Hz and 2.1nm RMS at
50 SPS isn't too shabby.  It wou= ld=20 be interesting to assume a seismic-mass
system and model how this woul= d=20 compare with commercial instruments and
earth-noise models.  I'm=20 betting it won't look so bad.
    Have you measured your environmental noise leve= l?=20 Is 2.1 nm a realistic target? The amplitude of the 6 second ocean microseism= s=20 may be from 500 to 15,000 nm!
<= FONT=20 style=3D"BACKGROUND-COLOR: transparent" face=3DArial color=3D#000000 size= =3D2> He=20 then goes on to describe the VRDT. I suppose for the VBB sensor this would= =20 greatly simplify the electronic design if one can deal with small sen= sor=20 gaps. I'm not sure about the noise. Does the VBB measure displacement= s in=20 the 1 =B1 nm range?   --- Just thinking out loud. I think it gre= atly=20 depends on what type of sensing one wants to do local, regional or=20 teleseismic.
      Amateur seismometers are usual= ly=20 limited by either microseisms or by environmental noise - we can't usually=20 choose a quiet remote site. I managed to reduce the noise of my LVDT to abou= t 7=20 nm for a 6 mm range at 10 Hz, but my environmental noise is much greater=20 than this.
 
<= FONT=20 style=3D"BACKGROUND-COLOR: transparent" face=3DArial color=3D#000000 size= =3D2>It would=20 be great to be able to use this with feedback.  No question that
= you=20 could use it for integral feedback, which mainly works below the low=20
frequency roll off (say, below 0.011 Hz).  You could make an awes= ome=20
integrator by digital summing, then feed back with a D/A.  Mid=20 frequency
range (derivative feedback) may not be practical.  Alth= ough=20 you could keep
your beam well centred with integral feedback, without=20 derivative feedback
at higher frequencies, you're limited by the +/- 1= ..0mm=20 (+/- 0.5 mm max, for
linearity) sensor gap.  I'm suspecting that=20 clipping levels in the
mid-frequency range are going to be the biggest= =20 limitation.
 
    So, we may need some 'lateral thinking'=20 here! There are 'problems that you do not need to have' - like:-
 
    The velocity feedback damping does not need to=20= be=20 generated that way!
 
    Neither do we need to use that troublesome desi= gn=20 of capacitative sensor!
 
 ***   You can use JUST position +=20 integral current / coil feedback if you ALSO have a quad magne= t +=20 Cu plate for the velocity damping! Trying to provide velocity damping by=20 differentiation and coil feedback is likely to very significantly increase t= he=20 overall circuit noise!  ***
 
    Regards,
 
    Chris Chapman

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