A three-dimensional position measuring system
Citation for published version (APA):
Driessen, F. P. G., Lucassen, F. H. R., & Ven, van de, H. H. (1988). A three-dimensional position measuring
system. In Theory of robots : selected papers from the IFAC/IFIP/IMACS symposium, Vienna, Austria, 3-5
December 1986 / Ed. P. Kopacek, I. Troch, K. Desoyer (pp. 433-438). (IFAC proceedings series; Vol. 8803).
Pergamon.
Document status and date:
Published: 01/01/1988
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+_ C o p y r i g h t O IFAC'fheorv of Robots, V i e n n a , A u s t r i a 1 9 8 6 INTRODUCTlON I n t o d a y ' s j - n d u s t r i e s , a n d o n t h e f a c t o r y f l o o r ,there is a fast growing interest in and usê of the
programble rulti-functional mnipulator or
ind6-trial robot. The industrial robot can be used
excellêntly as a fast and precise posiÈioning or
handling machine. However, in spi-te of its Mny
quaLi-ties concerning speed and precision, thê robot
also has its lini.taÈions. Due to the robot
dynam-ics, the positioning accuracy is inversely
propor-tional to the speed. Onê way of reducing Èhe
effect of the robot dynanics is to alter the ratio
b e t w e e n t h e m a s s a n d s t i f f n e s s , e . g . b y u s i n g n e w m t e r i a l s .
Ànother possibj,Iity is to dj-ninisb the negative
effects of the dynanics without changing the
dynm-ics thereelves. Now the aceracy and repeatability
of the nanipulator can be inproved by adiling sore
intelligence to the programed robot, i.e. by
changing its program j-n such a way that any
unwant-ed movemenÈ is compensatunwant-ed for. For thj,s, it is
essential that the dynamics of the robot arn axe
knom a pri-ori.
Recently, much attentj.on has been paial to the
anal-ysis of dynanic atructures of mnipulators (e.9.
À s a d a , 1 9 8 3 ; B o o k , 1 9 8 2 ) . o n t h e d e v ê l o p m e n t o f
dynanic robot models a measuring system with the
ability to reasure the position of a fixed. point of
the robot arm as a function of time could be most
useful. Such a measuring system could also be used
when checking robot perfomnce and validating
already developed models. T'lxe developrent of such
a s y s t e m i s t h e s u b j e c t o f t h i s s t u d y .
Basically, we are only interested in the position
of one point on the robot arm, narely the one at
the end of thê am, the Tool Center Point. various
m e a s u r e r e n t s h a v e s h o m ( e . 9 . B e l j a a r s , ' 1 9 8 4 ) t h a t
the most dominant eigen-frequencies are below 30H2.
These frequencies have a Mximl amplitude of
sev-eral m's. Furthermore, it has been shown that
most robot arns have a mximw acGracy of about
0,lm together wj-th a mxirum speed of 3 n,/s.
TOR-K
A THREE-DIMENSIONAL POSITION
MEASURING SYSTEM
F. P. G. Driessen, F, H. R. Lucassen and H. [f. van de Ven
Eirulhouen Unitersitt oJ Technology, Department of Electrical Engirtteing.
Measurement an(L Control Croup, PO Box 5lJ, NL-5600 NIB Eindhouen,
The NetherLantls
Abstract. when checking robot performnce, a measuring system with the abilj-ty to
measure both the static and dynanic behaviour of a roboÈ arm is essentlal. The system
can also be used to check on robot perfomnce and on valj-d.ity of already d.eveloped
mod.els. This device should be able to measurê the position of a fixed point on the
robot am, the so-called Tool Center Poj-nt, in three dj-nensions with an accuracy of
'lOpn,
together with a large scale bandwid.th of 30i{2.
The device uses three identical laser{pticaL distance measuring systere, each of which
measures the displacement of the Tool Center Point with respect to a reference point
belonging to that system.
Each distance measurerent system consists of a frêquency stabi-lized Laser, a tracking
systen and a laser interferometer, À useful laser stabilizatj-on basêd on theml
expansion has been developed, as well as an interferomeÈer detection unit and a
bj--directional interf erometer counter.
Kelryords. Àctuatorsi counting cirej-ts; data handlingi laser j-nterferometert position
controlr stabili-zationt tarcet trackinq.
l
l
Ii
l
It*
l
l 1From these data the followinq specificati-ons can be
extracted :
- a pos j-tiqn measuring acilracy of at least 10tn
with respect to all- three d.irensiore t
- a dynamic range of 0 - 5 m/s;
- a bandwidth of 0 - 100H2 for vibrations of very
smLl anplitude (a fraction of a nillineter)
and 30 Hz for aq)litudes of up to several
mil-l i r e t e r s .
Àt the rcment there is no comercial
three-di,ren-sional position neasurj.ng mchine that satisfies
these specifications. Therefore we decj-ded Èo
develop a (lov-budget) neasuring system ourselves.
PRINCIPIE
the objectives and specifications show that
in-dj-rect measurements, e.g. by detemining angular
positions of the motor axis, is inadêquate. By
using laser<ptical techniques it is possj-ble to
i-ncrease the measurenent accuracy. Becker ( 1984)
describes a system which uses two LaserbeaG which
are consÈantly projected at the Tool cente! Point
(TcP). The position of the TcP is detereined by
angÍular neasurement of the laserbeans and
triangu-lation. The achieved acsracy is about 0.lm and
is bound to the inaccuratê angular measurerents.
P f e i f e r a n d H o f ( 1 9 8 5 a , 1 9 8 5 b ) b u i l t a l a b o r a t o r y
prototype which uses four laser interferometers.
This prototl4)e produced some very satisfying
rê-sults. Due to these results, we decided to use Èhe
principle of 1en9Èh measurement by laser
interfero-neters.
The principle is depicted in Fig. 1. Three laser
j-nterferometers, situated at the rêference points
x l , x 2 a t d * 3 . . u " o t . t h e d i s t a n c e t o t h e T c P ( y ) .
309
t .
3 1 0
F. P. G. Driessen. F. H. R.
b )
Eig. 'la. The mêasurement
b . M e a s u r e m e n t o f
of length Li
p r i n c i p l e .
displacement D. instead
The lengths L1, L2 and L3 can be converted into the
coordinates of y. The describing equations havê
t w o s o l u t i o n s , y a n d y r . t h e l a t t e r b e i n g t h e i m g e
of y and rey easily be onitted by proper choice of
t h e t h r e e l a s e r i n t e r f e r o m e t e r s . I n f a c t , a l a s e r
-interferometer measures displacement instead of
length. It can be shom that if the coordinates of
a starting point p are knom beforehandr the
equa-tj-ons for deternining y have exactly the same form
as when using length measurement. By usj-ng a
seni-automtic calibration cycle the efforts needed for
setting up the system is kept to a miniM.
T h e p o s i t i o n s o f t h e r e f e r e n c e p o i n t s * t ( i = 1 , 2 r 3 )
can be calculated in a calibration cycle: one x'
takes the place of y and three knom different TCP
p o s i t i o n s / , 1 2 u r a - y 3 r e p l a c e x I , x 2 a n d x 3 .
In order to registrate the robot novements, a1I
three length, c.q. d.istance measurements have to b€
done period.j-ca1ly. with a sample frequency of 100
Hz the nost j.mportant eigen-frequencies (up to 30
Hz) can be determined.
THE CONSTRUCTÍON OF THE SYSTEM FOR ONE REFERENCE POINT
Àlthouqh Èhe complete system consisÈs of thrêe
identical length reasuring systens, we will focus
our attention on only one measuring systêm
belong-ing to one reference point.
Each length measurement system consists of a
frequ-ency stabilized laser, a tracking System and an
interferometer as depicted in Fig. 2.
À stabilized, laser frequency is necessary in order
to avoid node jurping and for the itrprovement of
the acaracy of the system. The trackj-ng systêm
will focus thê laserbeam at the TCP independently
of iÈs novements. Thê interferoneter counts the
displacem€nt of the TCP with respect to the
reference point in terre of half*avelengths of the
l a s e r l i g h t .
L u c a s s e n a n d F L H . v a n d e V e n
It wiLl appear that a very j-trportant part of the
systen is enbodi-ed in the retroreflêctor. This is
an optical instrwent with the following
quali-t l e s :
- the inconing and reflected beare are always
parallel, regardless of the incoRing angle;
- the distance beween both beare will change if
the centre of the retroreflector is mved
per-pendiolar Èo the direction of the fixed
in-contlng bean.
i n t e r f e r o m e t e r
F j - g . 2 . A s u b s y s t e m b e l o n g i n g t o a s i n g l e
reference point.
Figurê 3 shows two itrtplementatj-ons of the
retro-reflector. The corner cube or tripel is mde up of
three perpendicularly placed nirrors. The
so-called cats€ye consists of two half spheres with
the same refraction index but different radius.
1 x a ) F i q . 3 . T h e c o r n e r c u b e ( a ) r e t r o r e f l e c t o ï . b ) a n d ' c a t s - e y e r ( b ) LÀSER STÀ3ILIZÀTION
À laser constitutes the centre of the measurerent
system. In an interferometer an unstabilj-zed laser
cannot be used because' in qeneral, the spectrum of
the laser shows nore than one spectral line: the
Iaser modes. These modes are subjected to
frequen-cy drift, which my discharge into node-jwps, i.e.
complete vanishing of a mode and re-appearing at
another frequency.
Mode-jups should be avoided at any cost because
they influence all modes by changing the direction
o f t h e i r p o l a r i z a t i o n .
To prevent these negative effects, the laser should
b e s t a b i l i z e d . À s t a b i l i z e d l a s e r i s v e r y w e l l
-suited to interferential lengtsh measurement due to
its high light. intensity, j-ts smll divergence and
iÈs gEeat coherence length (the latter being
in-versely proportional to the sEll spectrum).
l a s e r s t a b il i z a l i o n
-fl. f2
, , [ ?
i
Éi:iï:i""*
A T'hree-dimensional Position Nleasuring S,vstem
I a s e r
c o n t r o l l e d c u r r e n l
. ) l l
F i g . 4 . T h e l a s e r D o p P l e r - p r o f j ' l e 9 ( f ) i n c l u d l n g
two laser modes.
In our experiments we used a 22 cm long He-Ne
plasm tube of 0'5 nW power. T'he wavelengÈh Ào of
lh. Ir"-n. liqht is apProxiEaÈely 6328 Á' The
am-plitude of the spectral lines fol"low a so-cal1ed'
Doppler-profile (t{aitland, 1969) which is a
Gaussian distribution around f^,
f ^ = $ ( c i s t h e s P e e d o f l i g È t a n d n t h e
.ËtraËÈion index). T"he modes can only exist if
they exceed a certain thrêshold t, see Fig' 4,
otheffise a mode-junP wil-L ocor' IÈ can be shom
that, alue to the chosen tube lengÈh of 22 o, the
successive modes are seParated by 685 MHz, so thê
Doppler-profile of about 1.2 GHz will screen two of
the modes.
one phenomenon which has not yet been fully
untler-stood is that the successive modes have a lineaÍ
perpend.icular Polarization' so they can be
seParat-ea ly polarizing filters. out laser stabilization
unit rust keep the two spectral lines uder the
Doppler-Profile until they have the same anplitude'
ro-àcco4>lisn this, it is necessary to measure the
difference of boÈh inÈensities' . The sPectral
fre-quencies of the laser are related to the tube
iengÈh. À length deviation AL results in a
fre-quency devi.atlon Àf as follows; At/f = -AL/L' This
neans, for exanple, that 0,05 pn tube exPansion
resulÈs in 1OO MHz frequency reducing' we have
chosen therÉI expansion as a vêry sinPle yet
effective way of adjusting the tube length. It is
irplemented. by a healing spiral mde of resistance
wire around the plasm tube. The control current
of Èhe spiral is provided by the dj-fference of the
intensities of both laser rcdes as staÈed above
( r i g . 5 ) .
To improve the PerforGnce of the stabilization a
PI (proportional and integïating) controller is
added. ï,ong term stability tests have strom a
stationary overall drift of 100 l4Hz which is, in
f a c t , q u i t e t o l e r a b l e .
Beat measurements also showed a repeatabj-lity
with-in 1OO MHz. The remj-ning frequency drift my well
be caused by drift in the fotodiodes or Èhe op-amps
i"n the Pl-controller.
THE TR,ACKING SYSTEM
For on-line distance measurements of a noving TooI
center Point the laser beam should be focused on
the TcP constantly'
The most effectj-ve way of achieving this is by
fixinq the laser tube and deflecting the laserbem
by means of a rotating mirror. since the TcP can
rcve in three dimensions, Èhe niror mst have (aÈ
Iêast) two degrees of freedon. The princi-ple of
the tracking system is ilLustrated in Fig' 6' In
swry, we distingui-sh a retroreflector attached'
to the TCP, a rotating mirror with its actuators, a
d.isplacement sensor, and a conÈroller. Ttre
track-ing system oPerates as follows. The distance
be-tween the incoming and reflected beaG at the TcP
will change if the TcP is rcved Perpendifllar to
the direction of these beaG. This novement of the
reflected bean will be spotted by Èhe sensor and,
j-n turn, the sensor wj-ll Provide control signals
which activate the actuators into rotating the
m.irror unt.il the reflected beam has reached its
original- position with respect to thê incoming
beam. lhe control-ler can be used to optimize the
D i O C € S .
F i g . 6 . T h ê T C P t r a c k i n g s y s t e m .
very high demnds are [Ede on the surface of èhê
niffor with lespect to Power loss, divergence' etc'
and on itg susPensj-on. In order to mj'nimize any
hysterese and (non-1i-near) friction, we have oPted
for cardan suspension with a fLexural pivot of
laninated springs. Four linear electromgnetic
dynamic transducers, two per degÍee of freedom' are
used as actuators for rotating the nirror' The
nirror and actuaÈors are nounteal in a heavy rigid
block of aluRinium. !{hen writing this article no
data about the transient response of this
deflect-ing uni-È was available'
c o n t r o l l e r
3 1 2
Basically, two types of displacement sensor can be
used, namely, a CcD-camera and a lateral
photo-diode. The latter is superior due to i-ts higher
speed, better resolution and because it
automti-cally indicates the centre of the bearepot on the
sensor .
THE INTERFEROMETER
The interferometer is the part of the system that
actualLy measures the displacenent of the TCp with
regard t.o Èhe reference point. In Fig. Z
retro-reflector À is atÈached to the (moving) TCp, and B
is a fixed reference retroreflector.
the interferometer is able to detect êvery half
wavelength (of the He-Ne liqht) dj-splacement of
retroreflector À. For thj-s, a harmonic
i n t e r f e r e n c e s i g n a l w i t h a f r e q u e n c y f r " o
proportj-onal to the velocity of the
TCÊ;-I zv_^- i
fr"o =
| --+- l, has to be detected. We are not
l " ^ l
only interested j.n the absolute value of Vr.D but
a l s o i n i t s s i q n . À s e c o n d l - n t e r f e r e n c e s i f r a : - ,
which is always present, my supply informtion
about the sign. In using a specially coated
sep-aration prism, a phase difference of plus or Enus
kn rad. depending on the sigm of VTCP will appear
between the two interference siqnalëi- This effect
i s i l l u s t r a t e d i n F j - g . 8 ( w i t h 0 = 1 / Í r a d . ) .
So the sigm of VTCp can be extracted flon the sigÍn
of the phase difference betweên both interference
s i g m a l s .
Fig. 7. The interferometer wiÈh two interference
beare.
To avoid rutua1 interference of the two laser
modes , one rcde has Èo be removed b1r reans of a
polarizj-ng fj-tter. À high-speêd photodiode is
indispensable for the detection of the interference
signal.s. The mximm frequency to be detected as
16 Mllz corresponding with the mxinum pemitteat ?Cp
velocj-ty of 5 n/s.
The obtaj-ned photo orrent is very difficult to
tackle due to Íts enormous dynamic ranqe of
0-161,Í12, its smll atrplitude due to opfical losses,
and a relatively high and unstable DC corDonenÈ.
In fact, thê intêrference sigmal is an
"ólitude
rcdulatêd signal wj-Èh a very sÈIl modulatj-on
index.
We have developed an interference detestinq unit
that converts the photo arrent into a useiul bLock
signal of the sme frequency and a constant
anpti-tudê. This detecting uit coqrrises, anonqst ;ther
things, a low-at filter with a mt-off frequency
of approximtêly 0.3H2 and a cosparator. ThL con_
parator is mde up of several cascaded ECL line
receivers. ECL, emitter coupled logi.c, is a loqrc
F . P . G . D r i e s s e n , F. H. R. Lucassen and H. H. van de Ven
f o i E j 0 ? t 3 , 4 : e i ( o . t - € ) ) , b r U : e _ I a ej ( o r r - 2 0 ) j ( o " t - € ) 9 : e F j - q . 8 . A p h a s e d i f f e r e n c e c a u s e d b y a s p e c j - a l c o a t e d p r i s m .
fanily that can be used up to very high frequency
( 1 0 0 I r { H z ) s w i t c h i n g n e t w o r k a p p l i c a t i o n s . W e u s e d
the line receivers as boosters and a Schnj-Èt
tri-gger. À laboratory prototlT)e of the detectinq
unit has given some very encouraging results.
For the detection of the pulses of the final rnter_
ference signall each representing a \À^
displacement, a counter is necessary. "
An up-down counter is necessary in order to repre_
sent the direction of TCp movements, thê counting
dj-rêction is mtched to the sign of the phase dif_
ference of Èhe two interference signals. Further
more, for dynanic operation, the counter contents
rust be sampled with a satrple tj-ne of 0. O 1 sec. , as
discussed before. A seven-decade .11 ttltz sanpled
bi--dj-rectj-onal counter with nÍcroprocessor càntrol
has been developed.
fhe microprocessor takes care of the saq)Iing,
storage of data, and the error handling. It my be
emphasised that for the complete system, one nicro_
processor can conÈrol all three interferometers.
MEÀSUREMEI{| ERRORS
AÈ various sÈages of the system, measulement errors
are introduced. Às stated i-n the introduction, the
total arcunt of errors my not exceed a position
neasurêeent. inaccurasy of 'l0pm. when dêfining a
measurerent work space of one cubic meter, the
mximum pemitted relative inaccuraclr is I 0 -5 . In
this case the rel-ative j-naceracy is defined
as the
absolute error in the position of ,Èhe T€p related
to the work space size.
In the following we will disass sone measurement
efiors.
The only measurenent error introduced by the laser
is related to its frequency drifÈ. The overall
drift of thê stabiu-zed laser is plus or mj-nus 50
M H z , È h e l a s e r f r e q u e n c ; b e i n g 5 . t O I 4 t t z , i r y I y r n g a r e l a t i v e e r r o r o f 1 0 - l .
The i.nterferometer causes several eryors to occur.
Íhe refraction index of the air, for instance,
directly related to the laser wave len+h. is nor a
constant but iÈ depends on, e.9. aÍr pressure,
vaPour pressure, tenperature and CO2 percentage of
t h e a i r .
Under norml circumstances this gives rj,se Èo a
relati-ve error of less than 10{.
The low-et filter of the interference detectinq
uniÈ also introduces an error. Very low Vmp
causes a very low interference frequency wfriètr can
1 , 2
-1
A T h r e e - d i m e n s i o n a l P o s i t i o n N l e a s u r i n g S y s t e m . ) l J
be filterêd out. Every sêcond that a low frequency
signal cannot pass the filter an error will occur'
when using a filter with a cut-off frequency of 0'3
H z t h i s e r r o r i s l e s s t h a n 0 . 3 x l l o = 0 . 1 p n P e r
second.. The period of time that thj-s type of error
occurs is probably a very smll fractj-on of the
Èotal arcunt of measuring time.
Ànother error rey be caused by the data handling'
!íhen converting the data into useful TCP
coordin-ates, numerj,cal errors are mde. However, these
errors can be mde sufficiently sEall by increasing
the accuracy of Èhe Processor.
Roughly speaking, the tracking systen causes three
types of êrÍorS. First we have the errors caused
by iqperfections of the Physical rêtroreflector,
i.e. Èhe mss corner cube or cats-eye' For the
Mss cornêr cube an optical Path length difference
appears when the angle of the incomj-ng beam
changes. T'his change in optical Path length
evid-ently results in a neasurement error'
For the cats-eye, the inconing and reflecÈing beare
are only parallel wtren there is a specifi"c distance
between them. If the inconing beam noves, the
reflecteal beam wj-Il no longer be Paraltel and this
causes a measurement error.
Reference uncertainty. As discussed before, the
reasurement Pri-nciPle is basêd on three reference
points. If the interferometer beLongj-ng to a
cer-tain reference Poi'nt cannot reasure a displacement
shen the TCP is noved on a sphere with that
refer-ence point as centre, the reference Point is
unam-biguous. Inversely, a reference point is
unanbigu-ous if all Points wiÈh equal oPtical' PaÈh lengÈh
are situated on a sPhere when rotatj-ng the mirror'
If Èhey are not on a sphere a measuremenÈ error
will occur when the eirror rotates'
The posj-tions of the reference points are
dêÈerman-ed by the raccidentalr Positions of the calibration
positj.ons during the calibration cycle' The extent
àf ttri" error is highJ-y dependent on the tyPe of
suspension of the roÈating nirror but is zero if
the turning point of the mirror coincides with the
beaming poinÈ of the Rirror, which we will call an
idêa1 rotatj-ng nirror.
Aining error. This error arises when the (ideal)
retroreflector is not correctly beamed due Èo
t r a c k i n g i l q r e r f e c È i o n s ( e . g . s l o m e s s ) ' I f t h e
inconing beam is not correctly fo$sed on the TcP
retroreflector, the dj-stance between the inconlng
and reflected beare wj-ll change, as will the
opti-cal Path length.
Ítle d.isplacenent sensor is abLe to detect this
êfrof-. iihen using an ideal rotating error, we
found that the aj'ning error can be calslaÈed
with the help of the error detected by the
disptacemenÈ S€nSor. In this sPecial case, the
aiming error can be comPletely comPenstated for'
CONC],USIONS
À three-dinensional Position measurinq system has
been presented. The measuring system can be
iÍplemented by three acsrate length or
desplacement measurements done by laser
interferometers .
As the total measurement system basically consists
of three identical subsystere we focused our
attention prj-mrilY on one sybsystem, mde up of a
laser plus stabilizationl a tracking syst4' and a
laser interferometer.
we devel,oPed a laser stabilization based upon
thelml exPansion which perforG satisfactorily'
In order to deternine the direction of the
displacement or velocity to be detected, an
interfêrometer princiPle with two interference
signals has Proved most usefull. For this PurPose,
a properly working high speed (17 lt'Hz) intêrference
detector has been designed and buj-lt, as well as a
sampled i-nÈerf erometer counter.
At the rcment the Èracking system, in particular
the rotating niror, j-s the bottle neck of the
system, due to the fact that it nakes high 'leEn'Is
on its nechanical construction and b€cause iuproper
design ÍEy cause considerable measurerent errors'
Ttre measurenent errors which are not introduced by
the tracking system are sufficiently smll with
r e s p e c t t o t h e p o s t u l a t e d s p e c i f i c a t i o n s '
Future resêarch will concentrate primrily on
invesÈigation of the transient rePonse of our
rotating nirror and on developing a mtched
controller in order to oPtinize the tracking
perf orMnce.
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