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Sommaire du brevet 2182627 

Énoncé de désistement de responsabilité concernant l'information provenant de tiers

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Disponibilité de l'Abrégé et des Revendications

L'apparition de différences dans le texte et l'image des Revendications et de l'Abrégé dépend du moment auquel le document est publié. Les textes des Revendications et de l'Abrégé sont affichés :

  • lorsque la demande peut être examinée par le public;
  • lorsque le brevet est émis (délivrance).
(12) Demande de brevet: (11) CA 2182627
(54) Titre français: APPAREIL PERFECTIONNE D'INTRODUCTION D'INFORMATIONS
(54) Titre anglais: IMPROVED INFORMATION INPUT APPARATUS
Statut: Réputée abandonnée et au-delà du délai pour le rétablissement - en attente de la réponse à l’avis de communication rejetée
Données bibliographiques
(51) Classification internationale des brevets (CIB):
  • G06F 3/02 (2006.01)
  • G09B 5/06 (2006.01)
(72) Inventeurs :
  • BARON, EHUD (Israël)
  • GENOSSAR, OMRY (Israël)
  • PRISHVIN, ALEXANDER (Israël)
(73) Titulaires :
  • BARON MOTION COMMUNICATIONS, INC.
(71) Demandeurs :
  • BARON MOTION COMMUNICATIONS, INC. (Etats-Unis d'Amérique)
(74) Agent: MARKS & CLERK
(74) Co-agent:
(45) Délivré:
(86) Date de dépôt PCT: 1995-02-03
(87) Mise à la disponibilité du public: 1995-08-10
Licence disponible: S.O.
Cédé au domaine public: S.O.
(25) Langue des documents déposés: Anglais

Traité de coopération en matière de brevets (PCT): Oui
(86) Numéro de la demande PCT: PCT/US1995/001483
(87) Numéro de publication internationale PCT: WO 1995021436
(85) Entrée nationale: 1996-08-02

(30) Données de priorité de la demande:
Numéro de la demande Pays / territoire Date
108565 (Israël) 1994-02-04

Abrégés

Abrégé français

Appareil d'introduction d'informations (10, 40, 50, 60, 70), comprenant un appareil (10) soutenu par le corps pour détecter des mouvements volontaires du corps et en donner une indication en sortie, un interpréteur (140) de symboles en sortie permettant d'exploiter l'indication en sortie pour fournir des symboles en sortie, et un interpréteur (140) de signaux de sortie de mouvements permettant d'exploiter l'indication en sortie pour fournir des signaux de sortie de commande de mouvements.


Abrégé anglais


Information input apparatus including body supported
apparatus for sensing voluntary body motions and providing
an output indication thereof, a symbol output interpreter
operative to utilize the output indication for providing
symbol outputs, and a motion output interpreter operative to
utilize the output indication for providing motion control
outputs.

Revendications

Note : Les revendications sont présentées dans la langue officielle dans laquelle elles ont été soumises.


46
C L A I M S
1. Information input apparatus comprising:
body supported apparatus for sensing voluntary
body motions and providing an output indication thereof;
a symbol output interpreter operative to uti-
lize said output indication for providing symbol outputs;
and
a motion output interpreter operative to uti-
lize said output indication for providing motion control
outputs.
2. Information input apparatus according to claim
1 and wherein said output indication represents features
of body motion including features which are characteris-
tic of the individual.
3. Information input apparatus according to either
of claims 1 and 2 and also comprising a mode selector
operative to cause a selected one of the symbol output
interpreter and the motion output interpreter to func-
tion.
4. Information input apparatus according to any of
the preceding claims and wherein said body supported
apparatus is a hand held device.
5. Information input apparatus according to any of
the preceding claims and wherein said body supported
apparatus is a generally pen-shaped device.
6. Information input apparatus according to claim
5 and wherein said generally pen-shaped device is opera-
tive to provide a visible writing function.

47
7. Information input apparatus according to any of
the preceding claims and also comprising an object whose
motion is controlled by said motion control outputs.
8. Information input apparatus according to claim
7 and wherein said object is a graphic object displayed
on a display.
9 . Information input apparatus according to claim
7 and wherein said object is a physical object.
10. Information input apparatus according to any of
the preceding claims and wherein said symbol outputs
represent alphanumeric symbols.
11. Information input apparatus according to any of
the preceding claims and wherein said symbol outputs
represent a sensory quality.
12. Information input apparatus according to claim
7 and also comprising a computer, having a location input
and a symbol input, and a display operated by said com-
puter and wherein said symbol outputs represent informa-
tion to be displayed on said display and said motion
outputs are supplied to said location input and are
employed by the computer to govern the location of said
information on said display.
13. Information input apparatus according to claim
7 or claim 12 and wherein said symbol outputs include
function commands.
14. A method by which a manipulable device provides
an output indication representing its own angular motion,
the method comprising:
recording actual acceleration data from a

48
plurality of accelerometers mounted in the manipulable
device;
generating predicted acceleration data on the
basis of hypothetical angular motion information;
comparing the predicted acceleration data to
the actual acceleration data;
computing improved hypothetical angular motion
information;
while the predicted acceleration data differs
significantly from the actual acceleration data, repeat-
ing the generating, comparing and computing steps; and
providing an output indication of the improved
hypothetical angular motion information.
15. A method according to claim 14 wherein the
angular motion information includes angular displacement
information, angular velocity information and angular
acceleration information.
16. A method according to claim 14 or claim 15 and
also comprising computing linear motion information from
the improved hypothetical angular motion information and
from the actual acceleration data.
17. A method according to any of claims 14 - 16
wherein recording comprises recording from at least four
accelerometers mounted in the manipulable device, wherein
the accelerometers each have a center of mass and wherein
the centers of mass do not lie within a single plane.
18. A method according to any of the preceding
claims 14 - 17 and also comprising receiving the output
indication of the improved hypothetical angular motion
information and manipulating an object in accordance
therewith.

49
19. An accelerometer array mounted in a manipulable
device and comprising:
at least four accelerometers each having a
center of mass, wherein the centers of mass do not lie
within a single plane; and
a manipulable device motion computer receiving
input from the accelerometers and generating an output
signal indicative of the motion of the manipulable de-
vice.
20. Apparatus according to claim 19 wherein the
manipulable device motion computer is operative to per-
form the following steps:
recording actual acceleration data from the
accelerometers;
generating predicted acceleration data on the
basis of hypothetical angular motion information;
comparing the predicted acceleration data to
the actual acceleration data;
computing improved hypothetical angular motion
information;
while the predicted acceleration data differs
significantly from the actual acceleration data, repeat-
ing the generating, comparing and computing steps; and
providing an output indication of the improved
hypothetical angular motion information.
21. Apparatus according to any of claims 19 - 20
and also comprising an object manipulator receiving the
output signal indicative of the motion of the manipulable
device and manipulating an object in accordance there-
with.
22. An information input method comprising;
sensing voluntary body motions and providing an
output indication thereof;

utilizing said output indication for providing
symbol outputs; and
utilizing said output indication for providing
motion control outputs.

Description

Note : Les descriptions sont présentées dans la langue officielle dans laquelle elles ont été soumises.


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IMP~VED I~)XM~TIO~ IN~VT ~PP~RATUS
~IELD OF THE INVE~TION '
The present invention relates to input device~
fas computer~ generally.
BACXGROUND O~ THE lNV~ ION
U.S. Paten~ 4,787,051 to-OlSon describes an
inertial mouse sy~tem which u6es three pair~ of a~cele~-
ometers.
U.S. Patent 4,839,836 to LaBiche et~ al. de-
scribe~ an appa~atu6 for ~roviding spatial orlentation
data ~lgnal~, U6~ ng an inertlal plat~orm acceleromPter
: cluster having a plurallty of aece~erometErs.
U.S. Patent 5,181,181 to Glynn descrlbe~ a
computer apparatus ~nput devlce ~or three-dimensional
lnfor~ation.
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SUMMARY OF T~E I~V~:;N~10~ -
The present invention seek~: to provide ~n
improved input device.
~ here ls thus provided in acco~ance ~lth a
preferred embod~ment of the pre~ent invention informatl~n
input apparatus includlng body ~upported ~pparatu~ f~r
sens~ng voluntary body mot~ons and provlding an outp-t
indicatlon thereof, a ~ymbol outp~t lnt~rpreter operative
to utilize the output indication fo~ providlng sym~ol
~utputs, and a motion output interpreter ope~ati~e ~o
utili~e ~he output indication ~or p~ovlding mot~on c~n-
t~ol outputs.
Purther in accordance w~th a prsferred r~ho~,i-
ment of the pre~ent invention, the outp~t indicat o~
represents feature~ of body motlon in¢l~di~ featu.e~
w~lch are character$stlc of the individ~al~
S~ill further in accordance ~lth a pseferredemhofl~ent of the present lnventlon, a mode ~elector ~
provided whi~h is operatlve to cause a selected one of
the 8ymbol outp~t interp~eter and ~e ~otion outp~t
interpre~er to functlon. .
~ urther in ~ccordance w~th a preferred émbodi-
ment of the present invention, the body suppo~ted app~sa-
tus is a han~ held device
Still further ln accordance wlth a prefe-red
embodiment o$ the pre~ent lnventlon, the bod~ suppo~ted
apparatus is a generally pen-shaped device,
Additionally in accordance wlth a preferred
e~bo~t~ent of the prese~t invention, the gene~ally pen-
shaped devlce is ope~ative to provide a vislble writing
~unction.
Still further in accordAncc ~lth a pref~rred
embodl~ent of the present invention, t~e informdtion
lnput apparatus also includes a~ ob~ect ~hose motlol ls
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cont~olled by the motion control outputs.
~ urther in accordance wlth a preferred e-~s~
ment of the present l~ventlon, the obj~ct is a grap~ic
object d~splayed on a di~play or a physlcal objeet.
Yurther in acco~dan~e with a preferred emb~di-
ment of the ~e~ent invention, t~e symbol outputs repFe-
sent alp~anumerlc 8ymbols or a ~ensor~ quallty such as a~
acou~tlc st~mulus, including b~t not limlted to music, or
such as a vlsual ~tlm~lus, including but not llmited to a
colo~ or a colo~ ~may~.
It is appreclated that ths applicability of the
p~esent ~nvention is very broad and is suitable for tbe
follo~ing field~ of use, inter alia: games such as v_deo
game~, toys, ~o~el veh~cles, robotics, simulation~ -uch
as flight slmulations, technical drawings and CAD.
Still further in accordance with a prefeirred
embDdiment of the present ~nvention, the in~orm~,tion
input apparatu6 also includes a c:o~puter, hav~ng a loc~-
tion input and a symbol input, and a di ~play oper~ted ~y
the compute~ and wherein the symbol outputs ~epr~8ent
information to be displayed on the d~splay and the motion
outputs sre s~lpplied to the lo~at~on inpu'c and are em-
ployed by t2~e ~omputer to govern the locatlon of the
~forma~lon on the ~splay.
Further ~n accordan~e ~ith ~ prefe~red e~odi-
~ent of tbe pressnt lnvention, the sy~bol output~ lrclude
unction commands.
There i~ al~o provl~ed, i~ accordance w~th a
p~e~er~ed embodiment of the pre~ent invention, a ~ethoa
by whi~h a manipulable de~lce prov~des an output i ~dica-
tion representing its o~n angular motion, the nethod
including recording actual accele~atlon data from a
plural~ty of accelerometers mo~nted in the ~anipulable
device, generating p~edicted acceleratlon dat~ cn the
~a6is of hypot~etical angul~r motion ~nfo~ma~lon, compar-
ing the.predicted accele~atlon data to the a~tual a~cel-
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eratlon d~ta, computing improved hypo~hetical angular
mot~on inform~tion, repeating, whlle the pred~cted occel-
eration data differs significantly from the actual accel-
eration data, the generating, compa~lng and co~put~g
step~, and providing an output ~dicatlon of the $mpro~ed
hy~othetical angular ~otlon information.
~ rther ~n accordance with ~ preferred emboCi-
ment of the present lnvention, the angular ~otlon in~or-
mation ~ncludcs ang~lar displacement info~matlon, angu.ar
veloclty informatlon and angular accelerat~on inforna-
tion.
Still ~u~the~ in a~cordance wlth a preferred
emho~i ~ent of the present in~en~ion, the met~od incl~des
computlng linear mot~on information from the improved
hypothetical angular motion in~orma~ion and from the
,. ~ actual acceleration da~a.
Addltionally in accordance ~it~ a preferred
e~bodlment of the present invent~on, recording lncludes
reeording from at lea~t four accelerometers mounted in
the manipulable dev~ce, w~erein the accelerometers each
have a cente~ of ~a~s and wherein the centers of masE, do
not lle within a ~ingle plane.
Stlll fur~her in B~co~dance wlt~ a pref~rred
e~odi~ent of the p~esent invention, the ~e~ho~ also
includes receiving the output indication of the imp-oved
hyp~thetical angula~ motion ~nformation and manlp~l~ting
an ob~ect in accordance therew~th..
There is additlonally provided, in accordance
with a pre~erred embod~ment of t~e present lnvention, an
accelerometer array mounted in a manipula~le devic~ and
~ncluding at least four accelerometers each havtng a
cen~er of ma~s, wherein the centers of mass do no~ e
within a s~ngle plane, and a man~pulable de~ice ~otion
compu~er recei~ing input from the ac~elerometer a~d
genera~lng an o~tput slgnal ind~catlve of the motl~n o~
the manipulable devlce,
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~ urther in accord~nce wlth a pre~erred embodi-
men~ of the pre~ent ~nvention, the manipulable devl~e
~ot~on co~p~ter is ope~ative to:
record actual acceleratlon da~ from the accel-
erometers,
generate predicted acceleration data on the
~asis of ~ypothetical angular motlon lnformat~on,
compare th~ predicted acceleration data to ,he
act~:l acceleration ~ata,
compute impro~ed hypothetical. angular mot~on
informatlon,
repeat, whlle the predlcted acceleration dlta
dlffe~s slg~ificantly ~rom the actual a~celeratlon data,
the generating, comparing and computing 8tep5, ~nd
provide an output ~ndication of the ~mproved
hypothe~ical angular motion lnformatlon.
~ urther in accordance ith a preferred embodi-
m~nt of the present invention, ~he apparatus also inc'ud-
lng an ob~ect rnanipulator receiving the output ~ nal
lndlcative of tbe mo~ion of the manip~lable devlce ~nd
manlpulating an obje~t $n a~cordance therewlth.
There is al~o prov~ded, ln accordance ~tl a
prefesred embodiment of the pre6ent invention, an in~or-
mation lnput method including sensing voluntary ~ody
~otlons and providing ~n output indication thereof,
utili~ln~ the output ~ndication for providing symbol
outputs, and utllizing the ou~put indication for provid-
ing motlon cont~ol output~.
~1 In~ TF .~ t lRULE 26~

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,
BRIEF DESCRIP~IO~ OP THE DRA~ S
T~e present invention wil~ be understood ~nd
appre~lated from tbe following aetailea description,
taken in con~unction wlth the drawln~s ln ~hich:
~ Fig. 1 ls a sl~pl~fled pi¢to~isl ill~strat_on
of object control and handwriting recognltion appara-u~
con~tructe~ and operatlve in accordance with a prefer:ed
embo~lment of ~he present invent~on;
~ igs. 2A and 2B a~e ~chem~tlc dra~gs of
preferred struct~re~ of portionæ of the apparatu6 of Pig.
l;
Pig. 3 is a simplified block diagram of tne
appa~atus o~ Pig. 1;
~ g 4 is a simplifie~ flow chart illustra lng
the ob~e~t control proces~ performed by the appa atus of
~ig. l;
~ ig. 5A i6 a si~plified flow chart ill~strating
the proce6s of step 4~0 o~ f~g~re 4;
~ ig. 5B compr~ses mathematlcal equations illus-
trating the proce~s perfo~ed by Fig. 5A;
Pig. 6 i8 a simplified block diagram of the
apparatu6 of ~lg. 1;
~ ig 7A i~ a simpllfied flo~ chart illustr-.tlng
t~e teachlng proce~s performed ~ the apparatus of Flg.
l;
Pig. 7B i~ a simplified flow ~hart ~llustratlng
the ~ecognition process performed by the apparat~s of
F~g. 1; and
Fig~. 8A ~nd 8~ are g~aphical illustratlons
u~eful in understanding a preferred method for a portlon
of the teaching and ~ecogn$tlon proce~es perfo~m-d by
the apparatus of ~lg. 1.
Appendi~ A i~ a co~pute~ l~st~ng of a ~refer~ed
software i~plementation of a portlon of steps 720 of ~$g.
7A and 800 of F~g. 79.
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D~TAILED DESCRIPTION OP PRE~E~EP E~IBO~IME~TS .
Reference ~s now rnade to Pig. 1 which is a
~lmplif~ ed plctorial illustration of apparatus operative
to perfo~ notion contsol ln synergl~lc combinat~on ~ith
~y~bol interpretation such a6 handwrlting recognitlon. A
hand-bel~ pen 10 is operative to be translated and rot~t-
ed abou~ some or all of three ~erpendlcular axes. ~he
term ~six degrees of freedo~" i~ ~sed hèrein to des~gnate
translation along and rotation a~out three orthogo~al
axes.
Pen 10 also comprlses a plurality of bullt-ln
accelerometers 25, such as model ICS 3031-2 comme~ei~,lly
available from IC Se~sors, 1701 McCart~y Blvd., Milp~tas,
CA 9503s. Prefsrably, pen 10 co~prlses.six accelerome-
ter~. 3rrang~d in pai~s, ~ith ea~h pair lylng alon~ a
part.. ~lar axis, with the axes being mutually orthogo~al.
Alter~atively, the axes may not be rnutually or~hogo~al.
In any case the accelerometers nsed not be coplana~.
Pen lO also co~prises a plurallty of ampli~iers
30, a~oc~ated with the plural~ty of accelero~eters 25.
F~g. 2~ ~s a schematic dra~lny of a p~eferre~ e~od~ment
of amplifler 30.
Alte~natively, removab~e apparatus compris.ng a
plu~ality of accelerometers 2S as descr~ed above, and
also C~ is~ng as~ociate~ ampl~iers 30, as deseribed
above, ~ay be retrofitted onto the pe~ 10. The remcvable
apparat~s may have the form of a cap fitting t~e erd of
the pen, a ring fitting ove~ the pen, or any other suit-
able ~o~m.
In a still fur~her alternative, the app.~atuæ
may not include a pen, but may h~/e any other su~table
hand held f~rm. In a yet furthe~ alte~nat~ve, the appa-
ratus ~nay be in the form of a ring fittlng the user' 8
finger, may be supported by the bod~ of B user, or mou~t-
ed thereupon in any ~uita~le matter.
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Pen 10 also comprise~ a ~wltch ~S, ~hlch ~an be
used to ser~d a signal lndicating whether pon 10 is bei~g
used for handwrltlng recogl~ition o~ as ~ pointing and
control devlce. Alternatively the slgnal may ~e sent ~y
moving pen 10 in a predef~ned format, or by any oth~r
appropr~ate means. D~ring handwritlng recognitlon, th~
user ~ay write with pen lO on wrlt~ng su~face 37.
The data fro~ the plurallty of acceleromete_6
25 in pen lo i~ ter~ hereln "ac~elerometer data". T~e
ac~elerometer data i8 sent through a aable to a contr~l
clrc~lt 40. ~lternatlvely, the accelerometer data msy be
sent through any suitable ~lreles~ communicatlon lirk,
such ~8 ultra80nlc, lnfrared, or by any other su~ta~le
mean~.
Control c~rcuit 40 amp~i~ie~ ~he accelerat_on
signals from pen lo and convert~ them to ~lgital fo_m,
preferably uslng aD analog to dlgltsl co-l~ferter. ~lg. Z~
~s a schematic drawing of a pseferred ~ A~ment of an
analog to digital ~onverter s~itable ~or the present
ap~licatlon .
Control circuit 40 then ~ends acceler~tlon ~ta
to a CPu 50. CPU 50 may be any sultsble CPU such as an
IBM PC ~ompatible co~puter wlth an B0386 p~oces60r ch p.
Asso~iated wlth CPU 50 are a s~een 60 an~ a
keyboard 70. An ob~ect 80, ~uch a~ a cur60r or a gra~h$c
rep~esentation of a ~hyslcal object, ls d~splayed on
~creen 60. When psn 10 i~ used for ob~ect control, CPU
50, ba~ed on the Acceleratlon data, move~ the cur60~ or
graph~c repr~sentation 80 with ~ix d~gree~ of fre ~om,
correspo-nding to the movement of pen 10.
A symbol 8s, such as one or more charactcr or
word~, may al~o ~e displayed on screén 60. When pe~ 10
is u~ed ~or handwriting ~ecognitlon, ~P~ 50, based on the
acceleration data, d~s~lays the ~ymbols corre~ponOln~ to
ha~ ls written on ~rlt~ ng surface 37 ol~ s~reen 60 .
The functionality o$ 'c~e apparatus of Fi g .
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will now ~e desc~ibed. U6ing switch 3~ the user ind~-
cates whether h~ndwriting recognition or object con rol
is to be performed. Depending on the user~ 6 choice, the
apparatus of Fig. 1 perform~ the approprlate function.
The functlonallty of the sppasatus of F~g.
w~en per~orming object control w~ll n~w ~e briefly de-
scrlbed. The user ~oves pen 10 in three dimenslons; the
motlon may ~ncl~de six degrees of frseaom~ Pen 10 sends
a¢celeratlon data ~e~slblng the acceleration~ of per 10
during the motion to control circu~t 40.
Control circuit 40 amplifies and digitizes the
accelsration data. ~he data i6 sent by control box ~0 to
CPU SO.
CPV S0 co~putes the tra~latior-..l displaoQment,
veloc~ty, and acceleration of pen 10 alon;~ three mut~ally
.. ; perpendicular axes w~ich axes nee~ have no relatlol to
the axes of the accelerometers. CPU 50 also ~ompute~ the
angula~ displacement ~rotation), ~elocity and acce_era-
tion of pen lo around the ~ame three mutually perpe-dic-
ular axe8.
E~sed on the computed output, CPU 50 moves the
cursor or the repre~entation o~ an object 80 on ~creen 60
~lth tran~lat~ons and ~otat~ons correspondlng to those of
pen 10. Th~ axes for the translation and sotat$on of the
c~rsor o~ object correspond to t~e a~e~ used to compute
the translation and rotation of pen 10.
Reference is now additionally made to P~g.
which ls a ~impllfied ~lock diagram of the apparat~s of
Fig. 1. Pen 10, whe~ moved by the u~er wl~h ~ix degrees
of fr~edom, trans~ts data describlng the a~eler~tions
of pen 10 to amplification c~rcult 120. Amplifl~atlon
c$rcu~t 120 a~plifie~ the ~cceleration data and trals~ltæ
the amplified acceleration data to analog/digital ~on-
verter 130. Analog/digital conve~t~r 130 dlgltize- ~he
accele~ation data and ~ransmit~ the dlgitized data to
displacement/velocity/a .leratlon ~omp~tation apparatus
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140, termed ~erein DVA 140.
DvA 140 co~putes the a~g~lar alsplacem*nt,
~eloclty, and aoceleration of pen 10 around three mutlal-
ly perpendicular axes which axes need ha~e no relatiol to
the axes of the aecelerometer6. DVA ~0 ~lso compate~
th~ translational displa~ement, velocity and accele~ation
of pen 10 along the ssme three mutually perpendicular
axe~.
DVA 140 transmits data describing the ~lx
degree~ of freedo~ to ~c~een display ~ontrol 150. Eased
on the data, screen display control 1~0 up~ates scr~n 60
to show the new location and orientation of the cursor or
the othcr ob~ect depicted on screen 60~
~ eference is ~ow addltlonally ~ade to F1~. 4
whlch ls a simplifled flow chart lllu6trating operatlon
of the apparatus of Fig. 1 in accordance wlth a pre~Prred
embodiment of the invention. The p~eferred method of
operation of the method of ~lg. 4 includefi the foll~wing
steps:
STEP 410; ~ead accelerometer data. Data from
each of the plurallty of accelero~eter6 25 1~ sa~pled,
preferably at a rate of one t~ousand data point per
secona.
STEP 412; ~heck whether sessio~ is at the
beglnning. A~ the beglnning of a ~es~on, ST~P 420,
described below, ~s requlrs~.
STEP 415: Check uhether pen i~ in motion The
accelerometer data is analyzed to determi~e whether pen
10 i~ in motlon.
Preferably, pen 10 18 considered t~ be n~t in
motlon ~henever all of the accele~ation s~gnals ln~icate
that the only sensed accelerations are due to grav$ty.
Signals are chose~ from one membe~ of each of ~hree palr~
of accelero~eters, each pair arranged along a dl~ferent
axis.
Let the vector U~(Ul,U2,U3) denote the -ignals

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of the three accelero~eters ~et the ma~ri~ A-(Ki,~;,K3)
denote the sen~tivities of each of the three accelero~e-
ters.
~ e sensit~vitie~ of the ac~elerometers co~rect
for any deviations of the axes of each palr of accel~rom-
etBrs as they are actually mounted in pen 10 from the
common axis on which they are supposed to be sltu~.ted;
this component of the sensitivlty ~s ~alled static sonsi-
tivity. The sensitivities a~so correct for devla_lons
between t~e axes o~ the global ort~ogonal coordinate
~ystem and the axes of the pair~ of acce~erometer~; thiæ
component of t~e sensitlvity is called dynamic senfiltivl-
ty. In actual practice, both statlc sonsltlvity and
dynamic . sensltivity may make i~portant contrlbutiors to
sensitiv1~y,
The statlc Eensltivlty i8 computed as part of
step 420, descri~ed in detail below. The dynamic ensl-
tivity ls computed 8S part of step 455, describ~d in
detail below.
Let ~ denote a s~all positlve conStan~ for
example, .OOSg where g denotes the a~celeration of ~ravi-
ty at the earth's 6urface. Then the pen i6 con~_dered
not to be in motlon whenever 1-6 C ¦ ~ lU ~
S~EP 420: Compute lnitlal condltlons. The
~nitial condition~ may compri~e the lnltial Euler .ngles
bs~ween the global coordinate sy~tem and the axes of t~e
pa~r~ of accelerometers. These Euler angleF are now
deter~lned.
Assuming tha~, at the inltial ~ondltion, either
at the beginning of the ~es8ion or when the pen ~8 not ln
~otion, the only acceleratlons measured are due to g~avl-
ty, the ~tat~c sensit~vity can be computed f~m the
accelerometer data while the pen is at re~t in three
known orientations. Alternatlvely~ the statlc s~n~ itl~i-
ty can be computed once ~s a prop¢rty of the pen a~d
stored ~or suture u~.
L~ ~DC!TITIl~r E ~ T /QI IJ F ~

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STEP 430~ Compute the diffe~entlal signa~ ~rom
each pair of accelerometeræ. The 6ignals fro~ ~ach
member of each pair of accelerometers are s~tracte~ to
form a 4iffe~entlal slgnal for eac~ p~lr of accelerome-
ters.
STEP 440: Compute rotationa~ parameters. ~he
rotational parameters def ine parameters of ~e mo~ion
about the three axes of the global coordlnate 6yS :em.
The rotat~onal parameter~ ~omprlse the t~ree E~ler
angles; the three a~gular ve~oclties; and the tlree
angular accelesations.
~ he ~otational paramete~s are comp~ted ln
parall~l usln~ an lterativ~ fè~h~k loop. In each
iteratlon of the loop, an estimated diferential acc61er-
atlon is computed from the current rotatlonal parameters.
If the difference between the estlmated differertlal
accele~atlon and the actual differentl~l accelerAtion
signal is less than a p~edetermlned s~ount, iteratio~ is
termlnated.
Otherwlse, new value~ of the parameter~ a~e
estimated in each iteration from the previous values and
the difference be~ween the est$mate~ dlfferential accel-
eration and the act~al dlffe~ent~al acceleratlon data.
~he method of this step is describe~ more fully ~slo~
~$th reference to ~lg. ~.
STEP 450; Compute translat$on acceleration.
The angular orientation and th~ angular accelerationl are
known from step 440. Yrom the an~lar o~ientatlo~ and
the sensltivlty vector the acceleratlon due to grav~ty i~
computed.
Given the angular acceleratlon a~d the accele~-
ation due to graYity as ~ell as the sénsitivity v~ctor,
the translational accele~ation i~ co~puted. The co~puta-
tion is according to the for~ula at~X lu-ag-ar whe-e at
is the tra~slatlonal accelera~ion; ~ is the sensi-ivity
vector; u is the signal of one accelerometer; ag 1- t~e
.~1IR~TIT~ C~ CT112111c~

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9snl43fi l~ 83
componen~ of the acceleration of gravity sensed ~y t~e
one accelerometer; and ar is the angular acceleratlon.
STEP 455: Vpdate dynami~ sensltiv~ty, As
explained a~o~e, the dyna~ic sen~itl~vlty repre ents
devlations between the ~xes of the global ortho o~al
cobr~inate system and the axes of the pairs of accel~rom-
ete~s. Since the angula~ orientation of pen 10 may ha~e
changed, ths dyna~ic ~ensitivity may ~lso have changed.
Gi~e~ e change in the angular orientatlon of
pen 10, the new dynamlc ~ensltlvity m~y be computed fro~
t~e new angular orient~tion and the old ~atrix of dynamic
sensitivity.
S~P 460: Compute translational velocity a~d
di~pla~ement. The transla~ional VBlocity is comput d by
lntegrating the translational accele~atlon ulth r~spec~
to tlme. ~he displacement is co~puted by ~ntegratir.g the
translational velocity wlth respect to ti~e.
STEP 470: Move screen ob~ect. Ba~ed or the
output of prev~ous steps w~ich comprises transla~ional
acceleration, velocity and displacement as well as angu-
lar accelesatlon, veloclty and orientation, the -creen
ob~ect i~ moved.. The moving of the screen ob~ect ~ay be
according to any appropriate transformation of th~ mo-
tions of pen 10.
Reference i~ now additionilly ~ade to ~iq. 5A
which i~ a ~lm~lified flo~chart illugtrating to ope-ation
of step ~40 of ~ig. 4. ~ig. SA incl~eæ the fol owlng
steps:
ST~P 480: Set initial pa~ameters. ~he rota-
tional para~eters comprise the th~ee Euler angles; the
three angular velocltles: and the three angular acc~lera-
tions. The initial value for the Euler angles i~ el~mput-
ea based on the previously ~nown val~e of the paramleters,
assum~ng that the acceleration has remained con~tanit.
S$EP q82; Co~pUte dlfferential acceleration
from model. Pirst the po8ition of an accelerometer 1
~ /nl ~1 ~ qc~

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the coordinate system of the pen is ceined by vector
and the rotation of the pen in the gl,obal coord nate
system is defined by a rotatlon matrix A(phl). For
example, A(phl) m~y be an appropriate ro~ation matri~ as
presented in ~ections 14.10-5 through'14.10-7, pag~s 475-
q8b of Mathematical UAr~ook for Scientlsts a~d Engi~eer6
by Rorn and Korn, 2nd Editlon, publl~hed by Mc~raw-Hlll
in 1968. Here p~i is a vector o~ Euler anqles:
phi~(~,B,r)T. Then the poslt~on of the ac,cele~omete_ in
the glo~al coordinate system R is deflned by RcAr.
Reference is hereby additionall~ ~a~e to ~lg.
SB, which contains e~uation6 useful for undcrstandin~ the
steps oP ~ig. 5A. Equation 490 lllus-rates the com~uta-
tion . of the accelerat~on of the .accelerometer in the
global coordinate syste~
As the Euler angles of the acceleronQte~
change, the sensltlvlty vector X al~o changes. The
change ~n the sensltivity ve~tor X ~ay be co~uted by
using equation 492 of ~lg. 5B.
Given the acceleration o the accelerometer and
the new sensitivity vector, the esti,~ated value for the
differentlal signal of the accelero,meter, ue~ may be
computed by using equation 494 of Pig. SB.
~ he remainder of the ~arame.ters may be co~p~ted
with an appropriate model. Preferjbly, a model ~h~ch
allows the use of only the para~eters speci~led above,
rather than a larger numbe~ of param~ers, is used. For
example, equation 496 of F~. SB rep~esents an appropr~-
ate model ~or computing the remainde~ of the parameters.
STEP 4~4: Is the difference between the com-
pu~ed and the current value less t~an a predete ~ned
amount? If the difference is less than thl~ amount, the
estimated param~ters are ~aken to bb correct and tera-
tion is termin~ed, with the computed parameters beiag
reported.
An appropria~e ~alue ~o~ the predete_m~ned
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amount ~nay vary depending on, ~or e~cample, the nla ~i~w
number of desired iteration~. One pQS~ible appropirlate
value would be . 0003 g, where g re~re~er. ~;~ the acce'lera-
tion of gravity ~t the earth ' s surface .
STEP 486: Compute changes in estlmated angle~
a~ording to the gradient ~nethod. New estimated ~,ngles
are computed by a~dlng a change to the old esti,mated
angles the change ~8 co~puted according to tbe gr~dient
method. The gradlent method i8 explained ~ore ful_y $n
sectlon 20.3-3 of Mathe~atical ~n~ook for Sc~ertists
and Engln~ers by Korn and Korn, referred to above,
STEP 488: Compute new paramete~s~ ~ew ~alues
for ~he re~aining parameters are domputed. Ite~a~ion
then continues with step 482.
The functionallty of the apparatus of ~_g.
when per'or~ing handwriting recog~ition will n~w be
br~efly .ascribed. Pen 10 sends acceleration ~ata
through. control clrcuit 40 to CPU 50. Teachinq and
recognition then occur based on the data from pen 1~.
Reference is now a2dl~ 11y ~a~e to Pig. 6
which is a simplified block ~iag,~m of the apparat~s of
~ig. 1 when used for hand~riting recogni~ion. The appa-
xatu~ of Pig . 6 receives lnput f rom psn 10 .
Pen 10, when movsd by the ~ser of the ~aJdwrlt-
ing recognition apparatu~, transm$t~ data describir g the
acceleration~ of pen 10 over tlme to acceleration teach-
ing control 630 and/or acceleration handwriting r~cognl-
tlon control 650.
The data from pen 10 may be transmit~ed to
acceleration tQachi~g control 630~ Transmission to accel-
eration teaching co~trol 630 typically occurs fo_- each
~erson ~ho is to use ~he system for handwritlng r~cogni-
tion for the first time. ~ransmls~ion to acceleration
teaching control 630 also preferebly occ~rs when r~3cog~i-
tion errors are d~tected use of acce~eration t~ach~ng
control 630 when recognit: n errors are detec~ed ls
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~ermed herein adaptlve teaching.
Acceleration te~ching cont.~ol 630 operater, on
the data rece~ ved, ~hlch data represPnts hand mo~enents
by the user when w~iting a 6ymbol, to~ether with ~P ~A~-
ly-provided identl~icatlon of the syl~ol co~e6 that are
as~ociated ~ith the data. Acceleratlon teachlng control
630 the~ updates databa~e 640, a pe=-person per ~ymbo~
acceleratlon dat~base. Database 640 co~ri~e~ proto-ype~
of accelerations for each symbol, com?rising ~ata ~ clf-
ic to e~ch per~on fos each sy~bol,
Alternatively, the d~ta f~om pen 10 may be
transmitted to accelerat~on handwritlng recogn$tion
control 650. Acceleratlon handwrit~g recognltlon con-
trol 6S0 operates on the data recei~ed from pen 1~ to
re~ognize the symbol represented by the mo~ement of pen
10 .
~ he o~tput of ac~eleratlon handwr~tlng re~ogni-
tion control 650 comp~iRes a li~t cf symbol codes! and
their respecti~e probabillties. ~n accele~ation hand-
wri~ing recognition post-processing ciro~lt 660, c~oo~e~
the co~ect symbol cod~ ba~ed on the li~t of symbol codes
and probabilit1es, and on post-proce~sing infor~atlon
whlch prefera~ly comprl~es a dstabaS~ of prevlous confu-
sions and a dictionary. The output of acceleration hand-
writing recognition post-proces61ng ~ircuit 660 i~ a li~t
of symbol codes and/or words sorted ~y likellhood.
Reference i~ now addltiona_ly made to Fig-,. 7A
and 7B ~hlch are simplified ~lo~ charts i~lust~at$ng
operation of the apparatu6 of Fig. 7 in a~cordance ~i~h a
preferred embodiment of the inventipn, when pe~forming
handwriting recognltlo~ Fig. ?A l~lu~t~ates the ~ea~h-
ing process and Fig. 7B illustrates the ~eco~nltion
process. The steps ln ~ig. 7A include the followln~:
STEP 710: Read accelerometer data. ~he ~ccel-
erometer data comprise~ data poln~s representing sa~pl~ng
o~ t~e acceleration mea~ured ~y accelerometers 25.
~1~u~ IIT~ ~u~c~r~

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Preferably, the sampling rate is appro~imately 1600 data
po~nts per second, averaged over 8 po1n~s, ~roducing an
output of approxlma~el~ 200 data polnts pe~ second.
ST~P 712: Identify pen-sur~ace ~ont~ct te-.mi-
nation The data from step 710 does not include the
surface contact ~tatus of pen lO. The ~ur~ace contact
status of pen lO may be der~ved from the accelera lltion
data as follows:
The acceleration data is filtered to re nove
co~ponents other than noise. ~o~ exanple, the accelera-
tion data may be filtered by a Butter~orth diqital filter
de6cribed in Diqital Filter Desio~ ~y T.W. Par~.~ ana ~.~
Burr~, John Wiley & Sons, 1987, chapte~ 7, 6ectlon
7.3.3, using the 4th orde~ lowpass digital filter wlth a
cut-off fre~uency of O . 7 to 0. 9 .
The flltered acceleratlon ~ata i8 the~ ..nte-
grated ove~ tlme. The slope of the integrated ~t l~ered
acceleration data is then snalyzea ~o determine th~ ~oint
at which the slope exceeds a thre~hol~ ~al~e. The ~o~ nt
at wh~ch the slope exceeds the threshold value i~ ~aken
to be the flrst point with status ~peh down". The ~oint
at which the slope falls below a thre~hold value is -aken
to be the first point with status "pe1 up~; the thre~hold
~alue may or may not ~e the same as the previously de-
scribed threshold v~lue.
The threshold values de~aribed above may be
determined ln advance for the partlcular type of pen snd
writing sur~ace, may be determined b~ a learning process
for the part~cular person, or may be de~ermined by ~ther
~ne~ns .
S~EP 715: ldent$fy 1nd1vidual ~ymbols and
words. ~he ~ata rom the previous step 18 di~i~ed lnto
~ata representing indivldual symbols. The status which
comprlses the status of "pen ~p" is termed hereln "pen
not down~. Prefera~ly, the num~er of consecutive data
points witb stat~s of "pen not do~n", whi~h data points
C!l 112C!~ITI ~TF .~ FT (RII~E 26~

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18
rcpresent a particular du~ation of the status "pen- not ..
down" i~ taken to lndica~e the end of a ~ymbol o~ o~ a
~osd.
Typ~cally, the duration of 6tatus "pen not
downr withln a range from 200 mllll~econds to 400 milli-
second~ is taken to in~ic~te the end of a symbol. Dlura-
tion of the statu~ ~pen not down~ ln th~ range from~ 800
milliseconds to 1200 milllseconds is typi~ally taken' t~
indicate the end of a word. .
Alternatlvely, the end of a sy~bol or of a word
may be ~ndicated by data polnts whlch represent pen
mo~ements that are not part of a sy~bol, or by ~ther
means. Outp~t data from ~te~ 715 co~prises ~ymbol end
and word end data.
STEP 720: ~ormalize accel~rometer data~ The
accelerometer data is normalized in tl~e or by other
means, Appendlx A is a compute~ llsting ln the C pro-
gra~ing language comprising rou~ine~ ~hat aro a pref~rred
implementstion of step 720. The routines comprise ~he
following routines in section II, "p~o pse~rocessing":
normal; toge~her wlth various deflni~ions used by roltine
normal .
STEP 730: ~ilte~ accel~omoter data. ~he
normali~ed ac~elerometer data received fro~ the prevlous
step i~ filtered ln order to remove noi~e. The f$1te~ing
may be accomplished by iteratlve ~moothlng of ad~accnt
point~ until the total change in the ~ignal ~ue to a
smoothing operation is less than t~e de~i~ed accuracy of
the data, or by other sulta~le means.
S~EP 740 Parameterize accelerometer data.
The data is parameterized according to crlte~ia which are
chosen .to ~epresent each ~ymbol. I~ the accelero~ete~s
are not m~tually orthogonal, the ~cceleration data ~ay ~e
~onverted into equivalent data in a mutually orthDgonal
coordi~ate system as follows:
Let the non-orthogonal slgnals be denoted by
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the vector u=(u1,u2,u3)T snd the orthogonal ælgnals be
denoted by the ~ector u~u~l~u~2~3l~ Then ~'~AoA 1u
where A is a vector of static ~onsitl~ity vectors
A-~A1,A2,~3) of the three accelerometers. The stat~c
sensitivity vector is compute~ from t~e outputs of the
ac~elerometers during a defined orientation without
movement. Ao is a dlagonallzed matrlx of sen~ltivity of
the orthogonal coordinate syste~ com~lslng the norm of
A1, A2, and A3.
T~e parameters prefe~a~ly compri~e the fo'low-
ing:
number o points ~efore nor~allzatlon;
~ormali~ed slgnal of pen stat~s
nor~alized signal o~ Z accel.eratlon;
slne of the angle ~' whlch ~ngle is define~ as
the angle between the vector assoclated with the current
data point ~AccXi,AccYi,~ccZi) and the AccXAccY plane as
shown in Pig. ~A;
cosine of the an~le a';
sine of the angle B' ~hich .angle is defin~d a~
the angle between t~e vector that conne~ts the polnt
before the prev~ous data point (AccXt_2,~ccY1_2,Ac~Zi_2)
an~ e c~rrent polnt ~AccX1,Ac~Yi,A~cZi), and the vecto~
that connects the cu~rent point with the point afte.- the
~ubsequent point (AccXi+z,AccYi+z,A~cZl+~) ln 6pace
~Accx~A~cy~Accz) as shown ln ~lg. 8B;
and cosine of the angle ~.
STEP 750: Generalize pa-3me~ers. ~he p~.ra~e-
ters of the symbol belng learned epsesent a fipe~lfic
lnstance of the symbol~ The symbol prototype stored ~y
the sy~tem is to represent the general ~haracteristlcs of
the symbol ~s drawn by that person. Therefore, the
parame~ers of the symbol belng learned are generalized by
some su~table means, ~uoh as by computatlon of the a~er-
age of the value o$ each paramete~ from previo~s in-
stan~eS of t~e symbol along with the value of each para~-
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~095~1436 r~ ~s/o-483
eter from the cu~rent instance of the 8ymbol .
S~EP 760: Update per-person per-symbol ac~el-
eratlon prototype database. The newly comp~ted par2me-
ters from the previous step are stored in the per-pe:son
per-symbol accelera~lon prototype ~atabase.
The steps in Plg. 7B lnclude steps ~h$ch ~ave
already been descrlbed above wlth reference to ~ig. 7A.
The remainder of the steps ln Flg. 7B include t~B fol_ow-
ing:
STEP 800~ For each prototype in the pes-person
pe~-~ymbol acceleration prototype d-.tabase, build a
measure of comparlson between the sa~le and the proto-
type, co~lned ove~ para~eters in t~e prototype. In
accordance with a preferred embodiment of the present
invention, all parameters are combined together to pro-
- , duce t~e measure of comparlson. Appendix A is a computer
listing in the C programing language domprising rou~ines
that are a preferred implementation of step 800. The
routines comprise the following, w~ich are foun~ $n
section ~, "sym~ols recognltion": ma~e corr; cor~el hem;
obj funct; togethe~ with var$ous definitions used by the
rou~i~es.
STEP 810: Create a list o~ probable sy~bols
sorted by likelihood Based on the ~easure or mea ures
of comparlson generated in 8~ep 800, a single 118.t of
probable symbol~ sorted by likelihood 1~ generated~
STFP 820: Chcose the corr~ct 8ymbolS and the
correct word based o~ the list, the databa8e of previous
confuæions and a dictionary. ~he symbols wlth gr~atest
llkelihood a~e the candidate8 f ro~ whlch the Correct
8ymbol is choçen.
The database of previous confusions provides
info~mation that allows the correc~i.on of t~e choi~e of
t~e correct symbol based on previous incorrect ide~tifi-
cations. The database of previous confusions comp_ises,
for each symboL, a li~t of other sy~bols whlch have been
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confused with tlle first sym~ol; for ~xa~ple, that. the
symbol " f " has of ten ~een confused with the symbol "b" ~
When ~uch an ent~y is foun~ comprising previous co~fu-
slons Ior a symbol in the 11st, the gymbol or sympols
that have previol~sly been con~uf~ed with the symbol ~n the
list are added to the li~t ~n accordance with the
p~evious example, if the sy~nbol "f " is found in tbe l~s~,
t~en the symbol "b~ is sdded to the list.
An indication of the en~ of each word ha~ been
passed as output since step 715, desc~ibed above. ~ased
on the ind1catlon, the mo6t likely word, comprislng the
most llkely identiflcations for each symbol in the ,ist,
is ldenti~ied.
The most llkely word 1~ checked against t~e
dictionary. P~ fera~ly, the dlctiona~y comprises bo~h a
general dictionary used for all u~ers of ~he system and a
~ersonal dictionary for each uses -of the ~ys~em I~ an
entry eXi6~S in the dictionary fo~ tbe most likely ~o~d,
~he word is cho~en a~ the correct identification.
If the most llXely word is not found in tl~e
dictiona~y, all possible ~ord co~binatlons in the li6t
are formed and eac~ is check~d against the dicticn~ry.
Among all such words ~hich are found in the dictlona~y,
the word wlth t~e highe~t likelihood i8 then chos~:n as
the correct ideDtification.
If none of the words is found ln t~e d~ction-
ary, the most likely wo~d is chosen as the corre~t lden-
tification.
. STEP E30; Check to ~ee lf a correction has
been entered. During the p~oce6s of re~ognltion, the
user of t~e syste~ is ~referably p~ovided with a vis~al
indicatlon of each symbol recogn~zed
~ fter the end of a word ls ~etected, the user
of the system prefera~ly is pro~lded with a visual indi-
ca~ion of the word recogni~ed~ The user ~ay irdicate
manually that a given word ~as incorrectly recognl2.ed and
~ T~TI ITI~ C!U~ 10~

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3~3 8821 RUG 1. 1996 6:16P1~1 #317 P.26
21~2627
WO 95Q1~3C r~ g51~ 183 ---
may lnp~t a correction.
STEP 840: Update databa~e of'previous co~fu-
sions, Based on a manua~ correction ent~red in step 830
or an auto~atic co~rection based on t~e dic~ionary, the
database of previous con~usion6 is up~ated. Based o~ a
ma~ual correctlon, the personal ~lct~onary ls al 60 u ~ at-
ed if t~e corrected wosd ls not ~ound in th~ dlction~!ry.
Preferred met~o~s and apparatus for handwr~ting
recognitlon are descrlbed iR the ~ollowlng appl$cati?ons,
the alsclosure of which i6 hereby lncdrporated by r~t~er-
ence: PCl'/US92/08703; Israel 104S7~ T nppllc-~lon .-
flle~ 31 January 1994 ln the US Recelving O~f~e ~y Ehu~
Baron and ~dward A Wolf e .
It is appreciated that t~e parti~ular embodi-
ment described ~n Append~x A ~s ~nten~ed only to pr~vldQ
an extremely detailed di~closure o$ t~e present lnve~lon
and i~ not intended to be lim~tlng.
- It is appreciatea that var~ OU6 features of the
i~ventlon ~lch are, fo~ olarity, descri~e~ in the con-
texts of separate ~rho~iment~ ~ay also be pro~id d in
com~ination ln a single embodi~ent. Conversely, v~riou~
features of the invention which ~re, for b~evity, de-
scrlbed ln the context of a single e~ho~m~nt may a_so be
provided separately or ln any suitable ~ubcomblnatlon.
It will be appreciated by pe~sonfi skill~d $n
the art that the p~esent lnventlon is not limltêd t~ what
ha~ been particul~rly shown and de~cribed herei7above.
Rather, the scope of the present invention is ~.ef~ned
only by the clai~s that ~ollow;
r~n IT~: C~FFT ~RI 11 F ~

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- 2182627
WO 9S/21-3G PC:TIUS95/0~83
23
APPENDIX ~
Recognition according . ~mbination Of signals
pefinitions and data 5trUcture~;
Board tl fil~
Function Init_datatr ( pottbase ) set~ con~munir ~` ~ n w1th date
translatio~ board via port portbase. It retl-ms:
O - colTnnunicaUon was es~u~l'~ed;
-1 - error on board (board ;~ not exi~
Mnt init_datatr ( int );
int ne~ ee ,~ ( void ~;
int read~ int channel, int ~ain );
Mnt read_point ( *truct polnt ~, Int );
/'int read_bl~ck ( struct p~int ', Int ma~_nurr~_poin~,
int time~ut_for_begin, int tirneout_for_end,
int key_mouse_stop ); ~1
Mlnt read_symbol ( strucl point ~, int, Int );
int mshit ( void ):
void close_datatr ( void );
~define PORT_BASE 0x210
A~derlne KEY_STOP 0x1
~denne llOl.JSE_STOP 0X2
#define l~EY_MOUSE_STOP 0x3
#denne PEI~_WAIT 0x1
~:define PEI l_NOW~lT 0x0
l~a~ ~ fil~
struct point_pen
unsigned ax;
unsi~ned ay;
unslgned az;
~nsi~ned pn;
struct point_~ablst
in~ x;
Int y;
Int p;
t~deline SYNCP~OBI r ox~o
~1 IQ~:TlTl ITF ~ ~ IRI 1I F ~

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2182627
woss/z1~36 . ]~ 153~rj 8j --
24
Da~r.H tile
detine PORr_BASE Ox210
de~ine CSR 0~0
..define GAIN Ox1
4deline DACO_LOW 0 ~2
:~deflne DACO_HIG~t Ox3
~de~ine l;~AC1_LOW Ox~
~de~ine DAC1_HIGH Ox5
#define CHANNEL_AX Ox4
~deffnc CHANNEI _AY Ox5
~define CI~ANNEL_AZ Ox6
#define CI IANNEL_PN 0
~define ST/~TUS Oxe
~derme CHANNEL_EMPTY OxO ,'
~define IDREGICTER Oxf
~define GAIN_1 OxOO
#dcflne GAIN_2 Ox40
~define GAlN_4 0~80
~de~ine GAI1~1_8 OxcO
~define IEP~ Ox21
#deflne IIR Ox20
ti!define IRQOOxOB
~d~fine IR01 0~tO9
#define IRQ2 OxO8
deSino IRC~3OxOb
define IRQ4 9xOc
~denne IR05 OxOd
~define IRQ6 OxOe
~define IRQ7 OxOf
/ struct poinS (
unsT~ned ax;
unsigned ay;
unsi~ned az:
unsigned pn;
I ;'l - :
~deflne ~INUS_PEN 1700
rOdefine PFN_UP Ox2
~define PEI~ DOWN Ox4
~define PEN_THRSLD 200
~define EMPTY
~define BUFS12E Ox80
..define TIME_COUNT 3000
#inelude <dos.h~
SUBSTITU~E SHEEr (RULE 261

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~^ ~18~627
WO 9~iJ2143C I ~ pr~ t3
~ier.H file
.. .. ..
Fl LENA~IE; SERIAL.H
Some detinitions used by SER.C
~1
~deline COM1
#define COM2 2
#define COM1BASE Ox3F8 t~ Base port address for Ct:~M1 ~/
~denne C~M2BAS~ Ox2FB r Ba6e port sddre6s ~or COM2
Tho 8250 UART has 10 registers a~o~. '7 ~hrough 7 pon ad~fe~i~s.
Here Qre their ~dd,~sse6 telative to COM1BASE and COM2B~S~, Note
thal the baud rate reglstcn, (DLL) and ~DLH) are actlve only when
the Divlsor-La~cl1 Access-Bit ~DLAa) is on. The ~DLAB) 18 blt 7 o~
lhe (LCR).
o ~XR Output data to the serial porl.
o RXR Input data from the serlal port.
o bCR Initiall2~ the serial porl.
o iER Controls Intenup~ generatlon.
o IIR IdenLfi s Interrupts.
o MCR Send contorl signal6 to the modem.
o LSR Monitor 1hG st~tus o~ the serial port.
s o NISR Receive st~tus of 1he modern.
o DLL Low byt~ ol beud rate divlsor.
o DHH High byle o1 b~-Jd rate divisot.
~/ .
Xde~ine TXR O r TransmN tegister (WRITE) ^/
#de~ine RXR O r Receive reglster ~READ) ~/
~:de1ine IER 1 /~ Interrupt Enable
:~define IIR 2 I Interrupt ID J
#deflne LCR 3 /' Llne control ~I
#deflne MCR 4 /- Mo~emcontr~l /
~detine LSR 5 /t LineStatus
:~deline MSR 6 r ModemStatu6 /
1~define DLL O r DivisorL~tch Low ~/
l~define DL~ 1 /^ Divisor latch Hlgh '/
I = .. .. . .
Blt valuss held in the Llne Conlrol Reglster ~l.CR).
blt n.-_n 9
0-1 00-5 bits, 01_6 blls, 10=7 bits, 11-8 blt8.
2 Stop bll~,
3 o-pa~ty ~ if, 1=parlly on.
4 O=parlly odd, 1_parlty even
Sticky panty.
6 sel break.
Toggle porl addresses.
, . I
~define l~lO_PA~ITY 0~00
#define ~VEN_P~RITY Ox18
#deline ODD_PARITY Ox08
SUBS71TU~F .C~JF~ ~

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WO 9.U21~36 2 1 8 2 ~ 2 7 P~9 101~83
26
E~it values held in the l ine Slatus Re~lster ~LSR).
bit m~aning
,,, .. ,....................... :
0 Dala ready.
Overr~n error - Data reglster o~ el..
2 Parity srror- bad l,~r.~lsslon.
3 Framin~ error - ~o stop bit was ~ound.
Break detect - End to tran6nl1~1un re~uestnd
5~ Transmltter holding register Is empty.
6 Tr~r,sr"i~tar shlft register Is empty.
7 Tlme out- off line.
~define RCVRDY 0x01
#detine OVRERR 0x02
~define PRTYERR 0x04
#dcfine FRUIERR 0x08
~define BRKERR 0x10
~define ~M~RDY 0x20
*deffne XM~RSR 0~40
#define TIMEOUT 0x80
r
Bit valuo~ held In the Modem Output Control Regi~ter (MCR).
bit meanln~
. .
O Data T~rrninsl Ready. Computor ready 1O 9c.
Request To ~end. Cornputer wants to ~end data.
2 a~l~al1a~ output ~1
3 ~uxlllary output #2.(~ote: Thls blt must be
6et to allow The cornmu, -qt: n~ cud to ~end
Interrupts to the system)
- 4 UART ouput looped back es Input.
5-7 not used.
tldefin~ DTR 0x01
#define RTS 0x02
~define MC_INT oxoa
Bit values held in the Modem Input Status np ~;t~r tMSR).
bit meaning
_ _
O delta t::lear To Scnd.
delta Data Set Raady.
z d~lta Rin~ 1n - r.
3 delta Data Carrler Deteet.
4 Clear To Send.
Data Set P~aady.
6 Ring Indlcator.
7 Data Carrier De~ect.
~define CTS 0x10
Jtceline DSR 0~20
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218~627
Wo 95t21436 I . 11-J: 3~ ~1483 --
27
Bit v~lues held In the Interrupl Ena~le Register (IEf~).
bit meaning
.. ..
0 Interrupt when data received.
Inlerrupt whcn transmltter holdin~ re~. ernpty.
Inlerrupt when data reception error.
3 Interrupt when change in modem slatus regls!er.
4-7 Not used.
. . I
#d~fine RX_INT 0x01
.. .
r . ~ .
Bit values held In the Inlermpt Iderlf~ . n f~e ,;ster (IIR).
blt meanin~
.
O Inl6rrupt pending
1^2 Interrupt IC) code
00~Change in mOdsm stat~ ro~ister
01-T,~r,~,..iller holdlr~g regls1er empty,
10=Data ~cel~..d.
11-r~c~ption error, or break encountered.
3-7 Not used.
., I
~defin~ RX_ID 0x04
ffde~ine RX_MASK0x07
These are the p0r~ ~d~lre~es ot the 825g Pro~ramm~bls Interrupt
Controller ~PIC).
~1 .
*define IMR 0x21 r Interrupt M~sk P~egister port '/
~d~tine ICR 0xZ0 1 Interrup~Control Port ~/
An end of inlerrupt needs to be sent to the Control Port ol
tho 8259 when a hardw~re interrupt ends
1
#define EOI 0x20 / End Of InterrL~pt I
The ~IMR) tells the (PIC) to sen~ice an interrupt only If It
Is not m~sked (FALSE).
1
#d~fine IRQ3 0xF7 r COM2 ~/
#detine IRO4 0xEF /~ COM1 /
The ~IMR~ t~lls th~ (PIC) lo ser~ioe an interrupt only If It
is not masked (FALSE).
1 .
~define IRQ3 01~F7 / COM~ J
~define ll~Q4 0~tEF r COM1 /
SUB~ JTE S~EEi (RUlE 26~

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~182!i27
~09~143C r~J~ 483
int llag; 2B
int SetSerlal~);
int SetOthers(lnt Porlly, in1 Bils, int StopBlt),
int SetSpeed(int Speed);
int SelPort(int Port):
void inTt_serial~v~
void comm_off(~old~;
void s~ (bll Pon. Int Speed, Int Parity, Int Bits, int Stop~11);
int putchpon~char);
void putstrport(char 3;
int 6oleh~ (vo~d);
vold offport():
S~rsonsl,H nle
r ~- . .
FILENAME: SERCONST.H
Sorr~ definhlono used by SER.C
The 82~0 UART has 10 reglslers ~ç~- ~le through 7 port addte~ses.
, Here are their ~d~ 2s rela~v~ to COM1BASE and COM2BASE. No~e
that th8 bsud rate reglstsrs, (PLL) and (DLH) are active only.w~en
the Divisor-La~ch A~s~ 81t (DLA~) Is on. The (DLAEI) i6 blt 7 ~f
1he (~CR).
o TXR Ou~put data to the serlal pcr~
o RXR Input data from the serial port.
o LCR Inl~l~llze the serlal port.
o ICR Controls lnterrupt generation.
o IIR IdenU,. s interrup~s.
o MCR Send eonto~ signals to the modem.
o LSR Mon~tor the status of tlle serlal porS.
o MSFt Recelve statl~s of the modem.
o DLL Low byte of baud rate dlvlsor.
o D~ High by~ of ~aud rate divisor.
. I
#defino TXR O r Tran6mlt register (VVRITE) 1
#define RXR O 1~ Recelve regi~ter (P~EAD) /
~define I~R 1 ~ Interrupt Ensble
#define IIR 2 r InterruptlD /
~define LCR 3 r Line control /
~define MCR 4 r r~Jlodem control ~1
*de~ine LSR 5 r Line StetlJs
.'tdefine ~SR 6 / ModemStatus ~1
#define DLL O r Divi60r Lalch Low /
ffdeffne DLH 1 r ~ivisorlatch Hioh ~I
~denne DLAB 0~80 1 ~/ :
Bit values held in ~he Linc Control Register (LC~).
blt meaning
. _ .
C!l It~CTlTI ITF .~I~E~ ~RUJ~ 26)

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WO 9SQ1~3G 2 1 ~ 2 6 2 7 ~ 9~lol~3
2g
0 ~ 00~5 bits, 01=6 bits, 10-7 bits, ~1-8 bl~s.
2 Slop bits.
S O-parity off, 1~parity on.
4 o_parity odd, 1=parity sv~n.
S Stidty parity.
6 Set break.
7 Toggle porl a~dresses.
/
..define NO_PARITY OxOO
#define EVEN_PARlTr 0~18
~doline ODD_PARI IY 0x08
.
Blt values held In ~he Line Sbtus Re~istsr (LSR).
blt me~nin~
O Dats ready.
Overrun error - Dela regi6~er ov~ r. .Illen.
Parlty enor- bad ~na"~sion.
3 ~ramino srror - No stop ~it was found.
4 Br~ak detect - End to tran~n.isSi~n requ~s~ed
Transmitter holdln~ re~i~ter is empty.
6 T,~h~".ilhr shlft rr~gister is empty.
7 Time out - off lino.
, #deline RCVRDY ox07
~define ov~ERR ox02
~de1ine PRrf~RR Ox04
.. detine ~RMERR ~xOB
"define BR~ERRoxl o
" de~ne XMTRDYOx20
~define X~.qT~SF~ 0~t40
~deline TIMEOUT Ox80
r " ,.
Bit values held in the Modam Output Control Register (MCR).
bi; me~ning
._.
O Da~a Tsrrr~nal Ready. Computer ready to go
Requsst To Send. Computer wants to send da~a.
2 auxlllary output ~1.
3 suxillarl/ output ~2.(Note: Thls bit must be
set to allow t, ;. comrnu., skn~ card to send
interrupts to the system)
4 UART ouput looped back as Input.
5-~ not usQd.
#detine DTR oxo1
~denne R rs oxoz
~define MC_INT oxo~
Bi~ values held in thc Modem Input S~atus Ro~ister (~SF~).
bil rnsaning
... . .
SUBSTITUl~ SHEET lRULE 26)

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X182627 -
WOssn~43fi ~ 9 Jo~483 --
0 delta Clear To Send.
delta Da~a Se~ Ready.
2 della Ring Ir ~ -rl r.
3 della Data Carrier Detect.
Clear To Send.
Data Se~ Ready.
6 Rlng Indicator.
7 Dala Carrier Detect.
.. , . . - /
~denne CTS Ox10
#define DSR Ox20
.,
r~
Bit values held in the Interrupt Enabh Re~ister (IER).
blt meanlng
O Interrupt when data ,t ~i d.
Inlerrupt when transrnitter holdlng re~. empty.
Interrupt wh~en data receptl~n error.
3 Int~rrupt when chan~e in rnodem 6htu8 re~7ister.
4-7 Nohlsed.
~. - 1
#detine P~X_INT OxO1
r . --
Blt values held in the Interrupt IdurC~c~ ;n Re~lster (IIR).
bil meaning
o Interrupt pendln~
1-2 Interrupt ID oode
00-Change in modem statlls re~ister,
01-~ransrnltter holding reglster empty,
- 10=Data .ecG~.~d,
11_re.,t ~tion error, or break encountered.
3-7 Not ul~d.
#define RX~ Ox04
#deflne RX_I~ASK Ox07
These are the port add,ess~s ot 1he ~259 ~luy,a~"..able Interrupt
Controller (plc~
1
~de1ine ~ R o~t27 1 Interrupt Ma6k Register port ~/
#define ICR Ox20 r Interrupt Control Pott
~n end of in~errupt needs to be sent to the Control Port of
the 8259 when o hardware inlerrupl ends,
/
~detine EOI Ox20 / EndO~ Interrupl /
SUaSTllUTE SHEEr (Rll~E26)

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~0 9Y~1~3~ 5-~483 --
31
The (IMR) ~ells the ~PIC) to sorvice an interrupt on~y l~ It
is not rnaskcd (FALSE)
1 .
nsi~ned char IRO[â~ 0x01, -0x02, -0x04, -0xB0,
_Q ~0,-0x /
~Sdefine IR~3 0x~, COM2 ~/
~define IRQ4 0x~F r COM1 '/
in~ SerSetPorlBase ( int, unsigned ~ );
int ScrSetSpe~d ( unsisned, long );
int SerSetBitsPari~ySlopBit ( unsigned . Int, int, In~
Int SerPutChar ~ unsigned, ~ d char ):
int SerPutSlring ( unsl~nod, u-- .ig~nd ehar );
Inl Serlr.i''`~rSter ( unsigned );
int SerGe~Char ( und~ned );
int SerTestDSR ( unsigned );
Int SerTestCTS ( unsl~ned );
/~ int nag;
Int SetSerial();
int SetOthers~inl Parity, Int Blts, int StopBit);
Inl setspeed(int Speed);
int SetPon(int Port);
void inl~_ser"~vs7ir);
void comm_of~(void):
void sel~llport(ln~ Port, int Speed, int Parlty, Int Bits, int ~t~Rlt);
in~ putchpon lchar);
void puts~rpor~(char);
int ~0tcnport(void);
~old of~port0;
'-1
T~hlel.~ flle
~dR1ine PI~N_DOWN
.. define PEN_UP 0
#define PE~_OUTPROX 09
~define TBL_WACOM_II 3
~define TBL_DATA_ASCII
J~define TBI _DATA_81~A~Y O
J~define TBL_MODE_S~REAM 3
1tdefine TBL_MODE_SUIITWI_STREAM 2
~tdefine TBL_MODE_SUBh~S5 u O
#denne TBL_MODE_POINT 0
#de~ine TeL_TYPE_ABSOLlJtE O
~define TBL_TYPEJRELATI~E
~defir~e TBL_MILLINIETERS 0
#define T9L_INCHES
#denne TBL_AI_WAYS_TRA~.'SMIT_YES
~d~Sin~ TBL_ALWAYS_TRANSMIT_NO 0
#d~fine 'rBL_BAUD_1 9200
Jldefine TBL_BAUD_9600 6
#deffne TEIL_E~AUD_4B00 5
#define Tf~L_BAUD_2400 4
fldetine TBL_E~AUD_~200 3
~dcrine TBL_8AUD_600 2
Jtdefine TeL_BAUD_300
~1 IR~TI~I ITF .~ rRI 11 1~ !~R~

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WO 9S/21~3G 1J~lru:~g~ 83 - -
32
~;de~ine ~E3L_~AUD_150
t;de1ine TE;l _PARlTY_r~loNE 0
~detine TE3L_PARllY_ODD
~de~ine TBL_PARITY_EVEN 2
~:d~1inc TBL_STOP81TS_1 0
#define TBL_SrOPBlTS_2
#detine TBL_DSR_IUO~JITOR_OFF 0
~defineTBL_DSR_~ONlTOR_O~ 1
~defineT~L_DATALENGTH_7 O
~dcfine~BL_DA~ALENGTH_8
~dofineTBL_TRANSFER_RATE_~AX 7
~delin~TBL_TRANSFER_RATE_~00 6
~de1ine TEL_TRA~SFER_RATE_67
#dofineTBL_TRANSFER_RATE_50 4
~dofineTBL_TRANSFER_RATE_20 3
#define T~L_TRANSFER_RATE_10 2
ffde1ine ~BL_TRANSFERLRATE_5
ëdefine TBL_TRA~ISF~ER_RATE_1 0
#defineTBL_ORlt31NLOG_UPPER LEFT
~define TBL_ORIGINLOG_LOWER_LEFT O
~deflne TBL_~ATA_TE~MINATOR_CR_LF 2
#define TBL_DATA_TERlullNATOR_LF
~de~ine TBL_DATA_TERMINATOR_CR 0
int read_poin~_tablet_pen ( unsigned, Int,
stNd poln~_teblet ~, 6truct point_pen 18~ );
int tind_se~pa~r.æt~r~_tablet ( int compon, unsigned 'pG~ Se ):
int ini~_tablet ( int port, unsigned ~on~ase, int cG~l".land_set,
int data_formEIt, Int oper~l;on_ node, Int orlgln_type,
int unit_mssure, int always_transmit, In~ spoed,
IM PantY, int stopbi: ~ Int dsr_monltot,
int dabl~ngth, int transfer_r8~e, int crlg_lo~,
in~ data ~,""~ ~tr~r, int ma~ t, in~ max_y );
vold clos~_tablet ( unsign~d potl~es~ );
SUBSTITUl~ SHEE1 (RULE 26~

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'~182627
... .
WO 9~121436 1 ~~ 1483 ---
33
I R~adina ~rom devlco
This procedure reads s~ hr ~ni~ed d~ta lrom ~he graphic tablct and acceler., .,ehl i r
nt read_point_lablet_pe~ ( unsigned pv~tb~se, int re~d_pen,
struct point_tablet tablst,
suucl point_pen p~n~8] )
int ind_paclcsge _ o, reply, debug~10~, I;
v,-siyl,ed ~har p:~agp~ = { O, O ~ O ~ O ~ O ~ O ~ O );
if ( lead_pen )
read_poin1_pen ( &penl0] );
l- O ;
Waltin~ for syn~hr~-bit ~r
do
if ~ ~ reply ~ SerG~tChar l pu.lbass ) ) c 0 )
retllrn reply;
debvg~ reply;
if ~ ~ P~ ll = (char) raply ) 8 SYNCROBIT
break;
) while ( ind_p~ e~ c 10 );
r Error ~ No synchro-bit In 10 bytes /
j~ ( ind_paCka~e ~10 )
return SER_SYNC1~081T;
I Read the next 6 bytes from tabht end 6 polnts from zcc.~l~r~l..e(tt /
lor ~ ind_package = 1; Ind_package c 7 ind_p~-~k;~e~ )
if ( read_pen )
read_point_pen ~ 8pen[ind_package] )
If ( ( rl~ply - SerGelChar ( po,l~_~ ) ) c o )
retum reply;
pa~Agelind--packa~] = (char~ reply;
I^ R~ad last point trom a~ e!e.v...eter
it ( read_pen )
read_point_pen ( &pen[ind_psclcage~ );
r Caleu -1es the values o~ the si~nals for table~ ~/
1able~-~x - ( p~ DPl0] & 0x03 ) cc 14;
table~-,x . = ( p~rlt-g~ lL 0x71 ) cc 7;
tablet-~x ~= ( pa; l ~ 2] 8 0x7l );
p~rl .ge~o] ~ 0x04
tablet-~x = table~-~x;
tabls~-~y ~ ( package[3] ~ 0x03 ) cc 14;
tablet-~y ~ ~ package~ ox71 ) <c 7;
tablet-~y ~= ( pa- ~3~t5] ~ û~713;
SIIR.~TITI IT~ .~HI;CT (Rl IJ ~

FRa~1:LRDRs PRRRY 2~ , T0: 613 230 8~21 ~UG 1. l~G 6:21P~1 #317 P.3~3
2182627
wo 9snl~36 . 1~~ 4B3
34
tablel-~p = 0;
il ( ! ( paeltage~o] & Ox40 ) )
tablel ~p ~ 99;
i~ ~ p4rkq~el3] ~ 0~04 )
lablet-~y _ - tablet-~y;
Il ( pAe~ set6~ & Ox20 )
~ablet-~p = ( pa~s~l6~ & Ox1t );
return 0;
)
GrA~ 9
/~ Two p.i~d ~s. Nonnalzation In time and Sllterin~ the lnp.~Jt si~na~s by mGoti.' ,ç
void normal ( int nu~old, ~loat arr_oldD, int num_ne~, ~loat arr_r~ewO
double koefl
in~ ind_old, ind_new;
koet~ - ~double) ( nurr~_old~ loat) ( num_n~w~ 1 );
Brr-new~o]t arr_old[0]
tor ( ind_nsw . 1; ind_new c nwTI--new -1; Ind_new
Ind_old ~ (int) ( floor ~ koeff ' Ind_new ) );
arr_new~lnd_new~ = ( ind_old + 1 - koeff ' Ind_new ) arr_old~ir d_old~
( koeft Ind_new ~ hd_old ) arr_old~ind_old ~ 1];
t an_newlind_newl = ur_new[ind_new];
arr_n~wllnd_newl = srr_oldlnun_old-1];
.
float smooth1 ~ int num ~ noat zD )
int ind;
nOat temp;
110at norma;
for (ind ~1, norma ~ O; ind c num - 1 ; irld~ ) {
temp = ~ z~hd -1]+z[indi+z[1nd+1~ 113.:
norrM ~= ~bbs ( ~[lnd~ - temp );
zEindl - tomp
reSurn norma;
)
.~1 IR.~TlTl ITF .~ ~ lRl~E 26~

~ DRS P~RI?R~I' c4GO~l TO: 613 230 8~21 RUG 1. 1996 6:22P~ #317 P.39
`- ~182627
W0 951Z143G ~,y"~ 83 ~ -
111. Pa~ame~er's e~trdclion
(`-q~ on of the parsmetcts or a symbol from the input si~nals ~/
int rnake_par ( char arg_ch )
s~ruct point 1
unsigned int x : 12;
unsi~ned int y : 12;
unsigned in1 ~ : 12;
U.IS;,~ ~d Inl pen: 4;
point, pointsl500];
Int read_noxLsymbol ( Fll E ~, ~truct pointO );
char f71e_narnel40~;
int lei , nurrber_poin1s c o;
f:ILE 'in_file, out_filel103, ~outJnUer , 'out bln;
tloat psraml6][NUMBER_POlNT], sum_part6][NUMBER_POlN~l;
int Indsx e O, max_point;
Int Ind, start;
in~ cur_x, r,~r_y, c~r_z, cur_p,
float arr_~MAX_POlNll, arr_ylMAX_POlN~, arr_ztMAX_POlNt~, arr-p~MAx-polN~
I~ Initiallzation of the resulls arrays to zero 'I
for(ind=O;lnd~6;ind~1 )
for t Index = O; index c NUMBEPl_POINT; Index4 1 ) t
param[ind]tindex] ~ 0.0;
sum_par[lnd~[index] - ;
?
r Id~r,ti~i atbn o~ the ~ile of data 'I
sprinn-t file_name, ~%o3d~smb~, [Int~ ~r~
it ( ( In_file -10pen ~ file_narne, ~rb~ ) ) c~ NULL )
strcpy (ext_err,file_name~;
ret-lrn -4;
stan o;
r Reading dats from file
while ( ( max_poin1 c read_next_symbol ( in_me, polnts ) ) ~ O )
for ( Index c O; indox ~ maX_point; index++ ) (
Qrr_xfindexJ ~ ~nOat) polnts'lndex'.x;
arr_y~lndex3 . ~tloat) points Index,.y;
crr_zlindex] ~ (:loat) pD!"ls';..dex,.z;
arr_p[indexJ - (float) ~ L-.d~ pen
arr_p~O~ = arr_p~ point 1] e 1
start~
nomber_points +- rnax_polnt;
J~ Calling ~he procedure n~ake_par_let for c~ parameters 1 6 1
make_par_lel ( arr_~, arr_y, arr_z, arr_p, param. max_point- 1 );
SUBS~ITUTE SHEEl (RULE 26)

FR0M:L~DP6 PRRRY ~4Ga~ T0: 613 230 ~21 RUG 1. 1~6 6:22P~1 #317 P.40
~- ~18~627 -
Wo 9sr2luG PC~T/US~ 1483
36
/~ Calculating the average o( each parameter ~/
~or ( ind ~ 0; ind < 6; Indl~ ~
~or ( index = 0; index c ~UMBER_POINT Index+~ ) (
surn_parlind]tindex] ~- param[ind3tindex];
..
for ( ind ~ 0; ind c 6; ind+~ )
ror ~ index = 0; index c ~UMBER_POINT; Index~ )
s~m_par{ind]~index] /- start;
5Urrl_p8t[0][0~ c (lloa1) numbet_polnts / ~tart;
fclose ~ in~tile 3;
r wr,lte 8Y9 in Binary file ~1
~printf ( file_name, ~3~ p- ~, (int) ar~_ch );
out_letter ~ fop0n ~ me_nerne, 'wb~);
tor ( index z 0; Index c 6; index~ )
1wrlle ( sum_par{index] . si200t(noat), NUM9EP~_POINT, out_lel~er):
fclose ( out_letter );
rell~rn stert;
void makE_,r~ar_le~ ( float ~rr_x~i, tloat arr_yO . flo~t ,arr_zD .
floa~ arr_pn, tloat paraml6371~UhllBER_POlN'rl, In~ rna~-poin1 )
. I .
noal end_smoo1h;
tloat neu~_arr_xl500], new_arr_yt500~, new_arr_z~S00] . new_arr_p[5301;
int ind, index;
r Call 1Or pr~ pr~.c~ssi,~ 1
normal ( mzx_point, arr_x, NUMBE~_POtl'~T, new_arr_x );
normal ( max_polnt, arr_y, NUMBE~_POINT, new_arr_y );
normal ( max_po~n~, arr_z, NUMBER_POII~IT, new_arr~
normal ( max_polnt, arr_p, NUMBER_POINT, new_arr_p );
max_point = NUMEIER_POINT;
for ( Ind ~ 0; ind ~ rnax_point; ind~ )
arr_x'ind = new_arr_~iinr~];
arr~,lnd, = new_arr_ylndl;
arr_z'ind - new_arr_z,ind];
arr_p,ind~- new_arr_p[lnd~:
~Ivhile ( ( end_6moo~h ~ srnooth1 ~ ma~t_polnt, arr_x ) ) ~ NIJMBER_POINT 110 );while ( ( end_smoo~h c smoo~h1 ~ max_polnt, ~rr_~ NUMBER_POINT I 10 );
while ( ( end_6moo~h = snlooth1 ( ms~t_point, ~rr_~ NUM8Ef;'~_POlNT 110 );
/^ Initialization of parameters ~/
psram[0 o _ ~floaS) srr_pl0~;
paramtl, ,o, - ( arr_~o] - arr_z[01 );
param'2 ,0, = 0.0;
param,3]!0] - o.o;
param,4~103 = 0.0;
pararr~3[01 = -;
~:1 IR~:TITI ~T~ HFFl ~RU~E 21i~

L~s PRRRY 246~959 TO: 613 230 8~21 RUG 1. 1996 6:23P1~1 #317 P.41
~ 2182~27
WO 95/2143G Pcsrus~ ol~u ---
37
param~OJ[1~ lo~l) arr_p~
/' C~lCL~ ;On 01 parameters 'I
param(1][1~ - ~ arr_2[1] - orr_z~o~ );
elev ~ arr_x~2] - arr_x~O~, arr_y~2~ - srr_y[O~, art Zt2~ arr_z[O~,
~pararnl2~l1), 8pararn[3][1
par4m[4~1) = O.O;
par~rn[5]~ O.o;
for ~ index - 2; Index c ma~_point - 2; Index~ ) I
param[O~lindex~ oat) arr_plindex];
p~ram[1]{~ndex] - ~ arr_ztindexl - arr_z[O] );
ele~ ( arr_x[index ~ lJ - arr_x[inde~t - 1], arr_ylindex ~ rr~ index 1l . arr_zlndex + 1] -
arr_z[inde~
&param[2~[indexJ, ~pararn(~]pndex~ );
an~les ( arr_x[index ~ arr_xrindex~,
arr_ylindex ~ 23 - ur_y[lndex],
arr_z~indsx ~ 2l - ur_z[indexl,
srr_xtlnde~] - arr_x~indcx ~
arr_ylindex] - atr_ylndex - 2~,
arr_zlindex~ - arr_z index - 2],
&param[~]~index~, ~pararn[5]tjndex] );
index_ index;
paramlOllindexl _ T'~at) arr_plinde~;
param!1J~index] ~_z[index] ~ arr_ztO] );
elev ~ arr_x[index . 1] ~ arr_xlinde~- 1], arr_yllndex ~ rr_ytindex 1J, arr_~[ndex + 11 -
arr_zllndex- 1] .
8paraml2][index~, &param~3~11ndexl );
~ param[4][index]~ -;
paramr~rlnde1t] - O.o
Index~;
r ~akul~tion o~ parame~ers for last point '/
param[O]lindex3 _ (float) arr_pllndexJ:
pa!aml1 [index] - ( arr_z[inde~t] - arr_zlo] ~;
parr~mf2 tindex3 = -:
psrarn~3,[index~ = 0-0 i
pr~r~ 4][index~ = O.O;
paraml5]tindex]- O.O;
)
/~ Proced~re nlev ca~rlJIates the SIN and COS o1 the an~le of el~allon '/
~oid elev ~ tloat x, float y, tloat z, tloat 'cos_Ug, tloat ~sin_ug )
lloat norma;
norma~t1loat)6qrl~x~x~y y~z~2)
il l norrna ~ .00001 ) I
'r os_U9 ~
'sin_ug 8 0.0;
return;
)
'cos_ug z ~ (tloat) sqrt ( x x ~ y ' y ) ) I norm~;
~sin ug = z / norma;
return:
)
SURsTITUTE SHE~T r~l IJ ~

LRD~S PRRRY ~4GO~ TO: 613 230 E~1321 fYJG 1. 1996 6:23P~1 ~317 P.42
~18~627
W() gS12143G ' I~ u;~ 1483 --'
38
/~ Procedure angl~s c~ os ~he SIN and COS of the an~le ~ ~t
void an~les ( lIoat x1, lIoat y1, noat z1, float x2, float y2, ~loat z2,
.flo~t cos_ug, noa~ '~in_u~ )
{
~loat normal, norma2, x3, y3, z3;
normal _ ( lIoat ) sqrl ( x1 ' xl I yl ' y1 ~ z1 ~ z1 );
normBz ~ l tloa1~ sqrt ( x2 ^ X2 ~ y2 ~ z2 - z2 );
;f ( norrna1 c .ooo1 il norrna2 c ~ooo1 )
.o;
's~n_ug = o.o ;
return;
~cos_U~ _ ( x~ y~ Zl ' ~2 ) / norma1 / norm~2;
X3 - ( yl ~ z~
y3~x2'~1-xl ~
z3=txl 'y2-x2'yl);
sin_u~ = ( (lloat) sqrt ( X3 X3 ~ y3 ~ y3 ~ z3 ' z3 ) ) / no~nal / norma2;
return;

FROM:LflDR5 PRRRY ~ æ~ TO:613 230 882l fWG 1. 1996 6:23PI-1 #317 P 43
~182627
WO 9~21~3G I ~ ~OIJR3
39
V Tr~inlna procçdures
r Procedure tor preliminary teacl7in~ '/
int first_teach ( void )
FILE ~1p;
FILE Ipout
int ~;
char bul~41 NdxStr[4], symholc[2F6]:
int ndx . O, max_symb ~ 0
Int num_sym;
CGI N~ r,~,1 ,9 data files, ple~se wait-,0,1);
It ~ hpen ~ 's~ ' rlat~, r'~ ) ) 2- NULL )
f
8trepy (exLorr,~ 1 ok rl7~
hlde_w, H ,e ~t (~con~erting data files, please W~ ,o);
return ~4);
~hile ( fscant ( fp, '%s', buf ) ~ 0 )
~ nb~i~[max_symt~t~] ~ bu1[0];
fclose ( Ip )
~pout-~open ("text adp','v~
~or ~ ndx 0; nd~ c max_symb; ndx~
sprintt ( 1~dxStr, ~%03d-, ndx ~;
: If ( ( nvtn-sym~make-par ( 6~."bol~[ndx] ) ~ ~= )
hide_comment ~conv~rti ~ data files, please walt-,O);
return (num_sym);
else lor ~I.O;icnum_sym;i++)
tprintt (1pout,-%c ,symbols[ndO
fclose (~pout);
hlde_co ~ e~ converting data flles, please ~alt~,O);
return ~0)
r prooedurefor ~ pt~tion olpr~.t~ ,es 1
float hu~e ~all_parl100];
int ~irst_sdsp ( Yoid )
(
float old_rec, n~w_rec
Int Goun~2o, ternp
char text;
char strtBOI
if ( ( temp ~ read_tex1 ("try txt~, &tex1 ) ) c O )
retun~ernp);
read_paranl l ~;
new_rec ~ rewgn ~ ^t~ prl', te~ct, O, o );
sprintt (slr,-%31-be1Orc cd~pl~tion-,new_rec);
commenl ~str,-1,1);
do ~

S PRRRY -hiO~ TO: 613 230 8~21 ~UG 1. 1996 6:24P~ #317 P.44
21~2627 --
WO95r2l~3c P~ ,g~GI~83
it (new_rec c o ) ~
hide_comment ~s~r,-1);
while ~ all_parllemp~ ULL )
fa~ee ( all_parltcmp+~] );
rellJrn ((int) neW_rec),
il ~ new_ree > .9g5 )
break;
dd_rec 8 new_rec;
new_rec = recogn ( ~try.prl-, text, 1, 0 );
i~ ~new_rec c ) l
hide,c~ln,nenl (str,-1);
v~hile ~ ailLpartternp] !- NULL )
Sarlree ( all_pzr[len,pw] );
return ~(int) new_rec);
hlde_a,,.u.,e nt (6tr,-1);
~print~ (str,'%3~- in ~ r t 1 n~,new_rec);
comment (str,-1,1);
new_rec = recogn ( "by.prl', text, O, O );
hide_c~.~,....er,t (~tr,-1);
sprintS (str,~,' 3f-aner adaption',new_rcc);
tom~en~ (str,-1,1);
il ~new_rec c O ) ~
hide_coml..ent ~str,-l);
whlle ( alLcarttempl 1- NULL ~ l
~ er~roe ( all_par~temp+~
return ((in~) new_rec);
}
~ whlle ( 'abs ( old_rcc - new_rec ) > .005 & covntt+ c ~ )
hidr~_cornment ~str,-1);
tarfree
while ( all_p~.[~mp] l~ NULL )
1arfree ~ pL~[t~
retum O;
SuBsTlTuTE .SHEf~ ~R~

FRO~:LRD~S PRRRY 21GO~ TO: ~182~327~ 8e21 ~ 1. 1996 6:24P~ #317 P.45
WO 95~ 36 I .~ ;101~83 --
41
V. Svmbol'S recogrlitiOn
stn~c~ point ~
unslgned int x : 12;
unsigned Inl y 12;
unsi~ned int z : 12;
unsignedlnt pen: 4;
) ;
struct reply
(
int ndx;
tloat WQi~ht;
~;
tloat reco~n ~ char 'file_pen, char tex~, Int adapt, int ~vc~rd~ )
(
11oat old_rec, new_rec, probs~l O][ZOJ;
int co~ t=O;
char syrrll~Q1~756], b~t[4];
unslQn~d long ttl;
Int max_symb;
FILE 'in_tite, ~file_symb, ~temp_word;
int symb;
unsigned long sta~ ord, end_word;
float paran~[6~[NUMBER_POl
int index = O, max_polnt:
strud reply repl;
int lemp;
int ~la~ ~d O;
int ind, NumSymbols ,ndY:
struet point symb_pnts lMAX_POlNT~
tloat arr-~qM~t - polNTl, arr_y[MAX_POlNl'l, arr_z[MAX_POlr~ . arr_p~MAX_POll~n;int mapl2561;
int order-O:
char lettersl10]~20],dict_wrds~10]~20]
Int end_o~_word-O;
int wrdlen;
tlDat ~umllOl,maxsum,ndx_maxsum;
char org_wrd(20~,t~ "JI~O];
Int t~_wldth;
in~ i;
If ( ( file_syrnb = fop~n ( ~sy"~bols dat-, ~r ) ) ~= ~ULL ) ~
6trcpy ~ext_err,~y.nbols.dat~):
return (-4);
70r (Ind-o;lndc256;1nd-f~) map[ind]c-1;
ma~symb- O;
~vhile ( fscanf ( file_6ymb, ~,' s~, buf ) ~ O )
(
~P [bu1~o]]~ -symb
5y~"l~ol;~[max-symbt~ - but[O~;
~closc ( file_symb ):
syrnbols[max_symb] = ;
~or ( ind _ O; Ind c 6: Ind++ )
t~l 1~,, ., r, r . _r ~_r ~

FR01~1: LQDRS ~t c4~ T0: 613 230 8~21 RUG 1. 1996 6: 24PI~1#317 P. 46
~182~2t7
Wo 9~143~ PCTlUS~ 3 --~
42
Ior ( ind~x = o; index c NUMBER_POINl; index~.~. )
pararn~ind]~index3 z o.o;
if ( ( in_fjlo c 10pen ( ~ile_pen, ~rb" ) ! =- NULL
..
strcpy (ex~_err,file_pen);
return -4
Indc~c ~ o;
~lumsymbols - 0;
symbs-1;
If (adPpt)
r~pl = make_corr ( param, r;ymbols, symb);
else (
repl, make_corr ( param, ~ymbols, -1);
1~ (repllo].ndxco)
return ( repl[0].wei~ht);
if (repll03.r.d~; sy..l~)
Ng~dl l;
else
Ngood _ Ng~od;
)
fclose ( in_Dle );
lumSy.~l~ols.;_0) return 0;
el~e return ~Ngood/(float)NumSy".~ols);
r C~lc~ n ot 1he ~imilaritv of all the parameters of ~ll the prototypes and the
syn~bol to be r~c~r~kgd l
extern tloat huge 'all_parl100~;
strua reply
(
int ndx;
fioat wei~hl;
~'
strltic Int comm_count = 0, abs_count ~ 0;
in~ obLtunc~ ( noa~ . Int, in1, float ~1003, ~loat p] . Int [10l );
float oorrel_hem ( ~loot [NUMBER_POINTl, tloat [NUMBER_POII~I" . float )
noat correl ( float tNUM~ER_POlN~ . noat ~NI IMBER-polNTi );
struct reply make_corr ( ~loat cur_parl6][NUMBER_POlN n, char 'symi~ols ,;nt symb)
tl~E 'cu~ le;
int ind_repl . ind_oorrct, ind, max_symb, ind_symb, Index;
struct reply arr_repll~0);
in~ arr_lnd[10];
float resl100], nresl7~, old_max_pnt - cur_p~rt03t03, com_wight;
rloat old_m~x_pnt2, corr~ 7], tmp~_par~6]rNUi~BER_POlNT];
char bu~[~];
int iterat
s~ruct reply n;
in~ i,j;
SUBSTITUTE SH~E~ rRI IJ F ~

FRa~i:L~S P~ ~ TO: 613 230 ~1821 ~UG 1. 1996 6:25PI~1 #317 P.47
- ~18~627
WO 95/~1436 rcTlusg~l483~~-
43
max_symb = strlen ( symboIs );
lor ( Ind_symb = o; ind_syrnb c max symb; ;nd_symb+~ ) (
~or(i-O;ic6;
for(j=O; jcNUMeER_POlNT;I+~
Imp_par[i]~1 z alI_partind_symb~ OO+j1;
if ~ ~mp_parlO~[O~ ~ o ~1
cur_parlO3~0] = old_max_pnt;
eo~r{lnd_symb3~N_PA~ 1.0' ~
min ( labs ( tmp_parlO~[O] - cur_parlO~tO] ) / cur-parto][ol, 1 ) );
old_max_pnl - c~lr_partO~lO~;
~rnp_parlO][4] ~1.;
cur-paqo~[o~
corrllnr~_syrnb~lO] = correl_hem t cur_parlOl, tmp_p~rlO], .~ );
tor ( Ind ~ 1; Ind c N_PAi~ -1; Ind~ ) ~
cotrllnd-symbl~ind~ ~ correl ( cur_parlIndl, trnp_par~ind3 );
]
)
else
for ( Ind _ 1; ind c N_PAR - 1; ind~+ )
corrlind_symb~rmd~ = 0.0;
)
)
if (symbcO)
, index = ob]_tunct ( cor. . ma~symb, hl_PAR, tes, nres, arrJnd );
Iterat=20;
else
f
sprintt ( bu7, ~%Q3d~r~ int) ar~ ollsym~
~ortlrO;lc6;i~)
tor ( j c O; j ~ NUMBER_POINT; J~ )
tmp-pertqo] ~ all_parlsymyD~1oo+Jl;
iterateo;
whlle ( (I"dax~obJ_tunct (eorr,max_syrnb,N_PAR,res,nres, arr_ind))>O
~ ~arr_lndtOp.~symb))
[
1f (iterat~1~) break;
for (Ind-O, Ind_corre~-O; IndcN_PAR-1; Ind++)
1t (eorrlsymy~lnd]~o.95 ' nreslmaJ)
Ind_corrct+~;
tor (index=O; index ~ NUMBER_POINT; index~+)
trnp partind]~index] = tmp_par [Ind][inde~q~.g
~Cur_par{inaJ~ de.~] `.1;
)
it (corrtsyrnb3~1ndlcO.g5 ~ nres~lnd])
ind_corrd~+;
Unp_partG]IO] = Imp_par~O]10~ ~ .9 ~ old_ma~_pnt ~ .1;
I~ (!ind_corrc
eral = ~u;
break;
. ) .

FROM:LP~S P~ ~'3 TO: 613 230 ~21 RLG 1. 1~96 6:25P11 #317 P.4~
2182627
W0 9.sl2l~36
44
iteral~
cur~parlO]IO)- old_ma~_pn~;
corrlsymbJlN_PAR-1]-1-fabs(tmp_par[O]~Ol cur_parlo]lol~/ cur_parlO~[O];
old_max_pn~ - cur_parlO~[O~;
old_rr~x_pnt2= lmp_parlO][O~;
tmp_parlol(o~
cur_par[O][~] = 1;
corr~symb~O~ c correl_hern ( cur_parlOl, tmp_par[o], 9 );
tor ( lnd z 1: Ind c rJ_PAR -1; ind+~ 3 ~
corr[syrnbl[ind~ - correl ( cur_par~lnd~ . tmp_p~r[indl ~;
)
cur_par~o~lOl ~ old_max_pn~;
tmP-p~rto]lo~ 5 old-rnax-pnl2;
r wnlie /
) r ~Ise '/
if ((Iterat~20) ~ ~index~O~ ~8 (iterabO))
(
cut_file = ~pen ( buf, 'w+b- );
fo~ ( Index - 0: Index c N_PAR,,1 Index l ~ ~
lwrite ( tmp_parfindex), skeof ( float ), I~UM3ER_POINT, cLIr_file );
tclose ~ cur_file
for(i=O,ic6;h+~
tor ( j = O ; j ~ NUMBER_POINT ; j++
all_par{symb]ll-100~D = trnp_par[
Index ~ min l index, g );
arr_ind!index~
~ res~rr_ir~l'..dcxn=-1;
~or (isO;jc=irlJex,l+~)
arr_repl[i].ndx.arr_ind~
arr_repl~i].wel~ht=-res[arr_ind[i3];
return zrr_repl;
)
I Ca~cul~ n of correlation bet~Ner~n two vect~r~ ~l
float co~rel ~ tloat tirst~NUMBER_POlNTl, float second[NUMBER_POlNn )
float sumxy = 0.0, surnx = 0.0, sumy - 0.0, sunlx2 = 0.0, s~!my2 ~ 0.0;
int l_d, I_s;
for ( I_s = O; i_s c NUMB~R_POINT ~_s~ ) (
sumxy += first~ s~condr_~];
surrLx ~_ n-stti-s1;
~surny ~_ ser~ond[i_ri];
~ mx2 ~ ~irs~ s] ' tirst[l_s];
sumy2 ~ second[i_sl ~ second[i_s~:
)
If ( ( 6urrlx2 - sumx ~ sumx / NUMBER_POI~T ) c O ll
( sumy2 sumy sù~ny I NUMBER_POINT ) ~ O )
return o;
il ( ( sumxy _ ( sumxy - sumx ~ sumy I NUM3ER_POINT ) I
ClIQ~!rlTIIT~ 1IJ 1 !~

FRa`1:L~DRS PflRRY ~460~ TO: 613 230 8~21 RUG 1- 1% 6:26PI~1 #317 P.49
WO ~Q143C 21 8 2 6 2 7 ~ J.,~ 4R3
sqn ( s~mx2 - sumx ~ sumx / I~lUMBER_PolNT ) /
sqn ( ~umy2 - s~)my sumy / I~ JIBER_POIN r ) ) c .~ )
re~urn O;
rell~rn sumxy;
/' Similarlty ~Jnction tor the parameter ot pen upldown /
tloat correl_her~ loaî par7[NUl~.~E~_POl~ , lloat p~rztNuMElE~ - polN~, noat b~rder )
in1 index;
~loat resull e 0.0;
~or ( index = 1; index c 1~IUM~ER_P011~1T; indsx 1 ~ )
result += ~abs ( parllindexl - per21index] );
result 1- ~UMBER_POII~IT;
result . 1 - result;
I~ ( re~ult c border )
retum P;
return result:
)
r Sele_t;on o~ the list of symbols that are likely to be the ~ymbol to be r~c~r,i~ed '/
int ob~_1unc~ ( tloat srrt100]p], int n_~yrnb, int n_par,
tloat res~100] . tloat nres~7~, im arrindex[30] )
' . ~ int ind_s, Ind_p, ind_arr = O;
: 110at max_res - 0.0, cur_res, abs_res = 0.0;
Int result_ -1
lor ( ind_s ~ 0; Ind_s c n_~ymb; ind_s~+ ) ~
10r ( ind_p = O, cur_res 0.0 ind_p c n_par; ind_p+~ )
eur_res ~= arrt.- ,_s]~lnd~
res[ind_sl ~ c~n_res;
I~ ( cur_res > m~x_r~s
resull = ind_~;
rnaY_rss c cur_re6;
abs_res = ma~_res ~ .85
d~ (
arrindexlind_an~] = result;
r~s[result3 ~ ~ reslresult];
for ( Ind_s = O, ma~t_res c O.o; Ind_s c n_symb; ind_s++ )
I~ ( reslind_sl ~ max_res ) (
resull = ind_s;
max_res_ res[lnd_~];
3 while ~ ma~_res ~ abs_res && Ind_arr c ~0 );
lor ( ind_p = 0 ind_p c n_par; Ind_p~ )
tor ( ind_~ = O, nres[ind_p] _ -5; Ind_s c n_syrnb; Ind_s~ )
nresllnd_p] - max ( art[ind_s~[ind_p] . nresllnd_p] );
rcturn ind_srr;
SUBSTITUTE SHEEr (RULE 2~)

Dessin représentatif
Une figure unique qui représente un dessin illustrant l'invention.
États administratifs

2024-08-01 : Dans le cadre de la transition vers les Brevets de nouvelle génération (BNG), la base de données sur les brevets canadiens (BDBC) contient désormais un Historique d'événement plus détaillé, qui reproduit le Journal des événements de notre nouvelle solution interne.

Veuillez noter que les événements débutant par « Inactive : » se réfèrent à des événements qui ne sont plus utilisés dans notre nouvelle solution interne.

Pour une meilleure compréhension de l'état de la demande ou brevet qui figure sur cette page, la rubrique Mise en garde , et les descriptions de Brevet , Historique d'événement , Taxes périodiques et Historique des paiements devraient être consultées.

Historique d'événement

Description Date
Inactive : CIB expirée 2022-01-01
Inactive : CIB expirée 2013-01-01
Inactive : CIB désactivée 2011-07-29
Inactive : CIB de MCD 2006-03-12
Inactive : CIB de MCD 2006-03-12
Inactive : CIB de MCD 2006-03-12
Inactive : Morte - Aucune rép. à lettre officielle 1998-12-09
Demande non rétablie avant l'échéance 1998-12-09
Inactive : Renseign. sur l'état - Complets dès date d'ent. journ. 1998-04-03
Réputée abandonnée - omission de répondre à un avis sur les taxes pour le maintien en état 1998-02-03
Inactive : Abandon. - Aucune rép. à lettre officielle 1997-12-09
Inactive : Lettre officielle 1997-09-09
Inactive : Lettre de courtoisie - Preuve 1996-12-17
Inactive : Lettre de courtoisie - Preuve 1996-12-17
Demande publiée (accessible au public) 1995-08-10

Historique d'abandonnement

Date d'abandonnement Raison Date de rétablissement
1998-02-03

Taxes périodiques

Le dernier paiement a été reçu le 

Avis : Si le paiement en totalité n'a pas été reçu au plus tard à la date indiquée, une taxe supplémentaire peut être imposée, soit une des taxes suivantes :

  • taxe de rétablissement ;
  • taxe pour paiement en souffrance ; ou
  • taxe additionnelle pour le renversement d'une péremption réputée.

Veuillez vous référer à la page web des taxes sur les brevets de l'OPIC pour voir tous les montants actuels des taxes.

Historique des taxes

Type de taxes Anniversaire Échéance Date payée
TM (demande, 2e anniv.) - générale 02 1997-02-03
Titulaires au dossier

Les titulaires actuels et antérieures au dossier sont affichés en ordre alphabétique.

Titulaires actuels au dossier
BARON MOTION COMMUNICATIONS, INC.
Titulaires antérieures au dossier
ALEXANDER PRISHVIN
EHUD BARON
OMRY GENOSSAR
Les propriétaires antérieurs qui ne figurent pas dans la liste des « Propriétaires au dossier » apparaîtront dans d'autres documents au dossier.
Documents

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Liste des documents de brevet publiés et non publiés sur la BDBC .

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Description du
Document 
Date
(aaaa-mm-jj) 
Nombre de pages   Taille de l'image (Ko) 
Description 1995-08-10 45 1 780
Page couverture 1996-11-28 1 17
Revendications 1995-08-10 5 168
Abrégé 1995-08-10 1 11
Dessins 1995-08-10 10 237
Dessin représentatif 1999-06-09 1 11
Courtoisie - Lettre d'abandon (taxe de maintien en état) 1998-03-03 1 187
Courtoisie - Lettre d'abandon (lettre du bureau) 1998-04-06 1 173
Rapport d'examen préliminaire international 1996-08-02 70 1 472
Courtoisie - Lettre du bureau 1997-09-09 1 19
Courtoisie - Lettre du bureau 1996-12-17 1 29