Onde rafde DATUM: OOCIJ4INTATiE ibliotheek van
nische Hoccho
DOCUMENAjT1: Ké'c_ 4? 'i3/V. Kostilainen, I.J. Sukselainen
MANOEUVRING TEST FACILITIES IN THE SHIP HYDRODYNAMICS LABORATORY OF THE HELSINKI UNIVERSITY OF
TECHNOLOGY
L-'431
sbouwkunde
13th INTERNATIONAL TOWING TANK CONFERENCE 1972
SUBJECT-NANOEUVRABILITY
MANOEUVRING TEST FACILITIES IN THE SHIP HYDRODYNAMICS LABORATORY OF THE HELSINKI UNIVERSITY OF TECHNOLOGY By V. Kostilainen and I.J. Sukselainen
Abstract
A new building for the Ship Hydrodynamics and Ship Structural Laboratories of the Helsinki University of
Technology was completed in December 1970. It comprises
two larger basins, manoeuvring and seakeeping basin of
mx
mx 3 mwith a towing basin of 130 mxli mx
5,5
m attached to it. The manoeuvring test facilitieshave been completed (finished) first, and are now in full
working order. These facilities include ultrasonic tracking system, model autopilot with several fixed
steering programs and necessary telemeter transmitting
and data logging systems.
Introduction
The original plans of the Ship Laboratories of the Helsinki University of Technology consisted of a conventional
towing basin of abt 200 m length. Later, plans were
changed to correspond to the requirements of actual
research projects. The length of the tank was reduced to
130 m and a manoeuvring and seakeeping basin was included
to the final plans. In addition to these, the facilities
will comprise an atmospheric circulating water channel of composite concrete-steel construction with a measuring section of 1,5 m x i in.
Until now model tests have been made with free running
models of 3,2 - 3,5 in length. This model size seems to
-2-for measuring equipment and batteries and the limitation of scale effects. On the other hand, this model size has
proved to be the maximum with respect to the size of the
basin. Thus, in the light of experiments made this far, the size of the manoeuyring basin, 40 in x 40 m x 3 m,
appears to be a suitable solution both from the economical and model testing technical points of view.
Arrangement of the basin
General arrangement of the basin is as shown in Fig. 1. The manoeuvring basin 40 m x 4O ni is connected to the
towing basin by an approachway of 6 mbreadth. Water level at maximum depth of 3 m is the same as the normal water level in the towing tank. When manoeuvring tests
in shallow water are made, the approachway is closed by a floodgate of floating type and the water level in the towing basin can be kept unchanged.
The bottom of the basin was precisely levelled for shallow
water experiments. An ordinary reinforced concrete bottom was cast abt 3 cm below the designed bottom level. By means of a net of precisely levelled brass studs a layer of concrete of low cement percentage was then laid and
finished to the exact level. The evennies of the bottom was checked by systematically running a model very slowly at shallow water. Clearance between the bottom of the model
and tank was measured by means of a modified ultrasonic
wall thickness gauge. According to these measurements 95 % of the area of the bottom is at the same level within
accuracy of 1 mm. Maximum deviations in the::'rest 5 % are of the order of 2 mm and these areas will be levelled in connection with the next emptying of the basin. Though
the tracking of the model is carried out in the first place by ultrasonic method, there' is a photographing platform
13.6
in above the tank bottom. The rails of the overhead crane of the model work shop have been extended 3 in overstructures used in the tests.
A plunger type deep water wave maker of 4O in length iil be built on one side of the tank. A removable flap-type shallow-water wave maker, which has a maximum length of 20 in, is now under construction.
Model Position Plotter System
The system determines the rectilinear coordinates of a
free sailing ship model the maneuvering basin by
ultrasonic distance measements, using a digital
coordinate computer. The path of' the model is plotted
on a X-Y-plotter and simultaneusly recorded on punched
tape by the data logging system of the tank. Tha basic
design was done by K. Luukkonen when working at the
Applied Electronics Laboratory of the University. He was also responsible for constructing the original equipii'ent.
By measuring the distance to a model from three or four
corners of a square basin with a side length a, the
expressions for the X- and Y-coordinates can easily be computed without using trigonometric functions. Thus
r r
a"3"+a
X
2a 2a
r r
a r xj a
The distances r1 are measured by using ultrasonic pulse, which is transmitted at known instant from a model borne ultrasonic transmitter and received by four appropriate receivers situated in the corners of the 0 in by 40 in
manoeuvring basin. The transmitter is sending pulses on
radio command from the centx"al unit ashore. At the
instant when the pulse is sent, the computing of the square of' the distance in units of 2.a at a frequency
z'
flow structure of which is shown in Fig. 2. When the
ultrasonic pulse reaches anyone of receivers; UR, the
contents of 12 most significant bits of the distance in
SQR is transferred to the corresponding register DR. The initial values of XR and YR are set by the LCU to be
equal to 210. Three of four distances in DR are selected so that the longest distance is rejected. The
data selector directs the two necessary square distances
for each coordinate to XR and YR respectively. The LCU
controls the additions and subtractions in the XR and YR
registers according to the equations. For an analogue
X-Y-plotter the computed coordinates are converted to
analogue voltages. The coordinates are simultaneously
recorded by a data logger on punched tape.
The position plotting can occure at frequencies of 4,2,1
arid 1/2 Hz. The Working frequency of the ultrasonic part is 124 kHz. The transmitter and the receivers use
piezoelectric radially polarized ceramic tubes (Brush
Clevite PZT-5 H) located vertically. The receiver signals
are amplified at tank corners by 80 db amplifiers feeding
long transmission lines to the central unit. The error
in the positioning is suppdsed to be within ± 20 mm.
Model Autopilot System
For precise and repeatable model manoeuvring an automatic rudder control unit is desirable. In our labòratory the
problem has been solved by constructing a special digital
control unit actuating the rudder by a stepping motor.
Mr. J. Kangas from the Applied Electronics Laboratory has been responsible for the design and construction of
the unit.
A functional block diagram of the system can be seen in Fig. 3. The automatic steering modes are as follows:
5
- trapezoidal steering
-
Z-marìeuver
-
constant heading constant course rate - Nomoto parallel shiftIn addition, a hand control mode is provided. The program
required is pre-selected before each run and the model is launched under
manual
radio control. The ptogram is thenstarted by radio and after the experiment the model is returned to dock by hand steering. All program parameters
are pre-set by digital selector switches at the front
panel. The rudder is turned in steps of 0.08 deg. During a run the rudder can be centered automatically at will.
General instrumentation
The models, which use NiCd-batteries as power suppliers, can be equipped with all necessary gear. The instrument-ation
includes
coLrse-, course-rate-, heel-, and trimgyros,propeller dynamometers, speed logs, echo sounders for
shallow water etc. The measured data is transferred to the data logging station ashore by a 8-channel
FM-FM-telemetry system. The received data is normally scanned
along with the model position coordinate values by a
data logger. The data is then punched on paper tape at
a maximum rate of 75 characters per second. For higher
data rates the telemetry system also allows the measured values to be recorded as FM-multiplex on magnetic tape
for subsequent processing. The reduction and analysis of the experimental data is accomplished by an Univac 1108
computer in the State Computing Center. The computer is
also accessible through a slow time-sharing terminal in
GATE
r
1L
L.J
MODEL ORK SHOMANOEUViÑG BAS
I ¿0mi'
O 10mSID (2)
-UR1 UR2 SIR 24 bits-'
SQR 24bitsF-DR i DR 2 DR3 0R4LOGIC CONTROL UNIT
IXR
h-j XBR
2bits
j D/tA converter YR LC U I YBR 12 bits ID/A converter
I
6i
'V- LIMIT FOR Z - STEERING
0
SUMMATION SW ITCH 6max 'V- 'Po Q - .4 COMPARATc* L FIG 3. MODEL MANEUVERING AUTOPILOT BLOCK DIAGRAM S IGN SENSOR
I
RUDDER ANGI.E COU N T ER STEPPIN6 MOTORi..
I. LIMIT SWITCHES 4 PERIODIC STEERING-FREQUENCY FREQUENCY SWITCH
DIRECTION SW ITCH
M ANUA L STEERING BY R,'
SINE AMPLITUDE
A
_J AMPL
r
SINE MEMORY SWITCH
i
BRM MEMORY CONTROL INITIAL MODE SOFFSET DUR ATIO__
i CONTROL F R 0M RADIO CONTROL
Q-..
10Hz M1 12 BIT 'V MASTER sLOW PASS FILTERS