331
1 INTRODUCTION
1.1 Problemdescription
Duringthelastcentury,theshareofmaritimetradein
thetotalvalueofworldtradeisconstantlyincreasing.
Nowadaysmorethan90%oftradeisestimatedtobe
transported by sea (EMSA 2015). This statistics
portrays also that the world oil tanker account for
ab
out30%ofglobalseabornetrade.Throughtheuse
of new technology of shipbuilding, modern
navigation and control systems, shipping in the
worldʹs become more secure. Despite this, the total
number of ships involved in accidents is still large.
Theaccidentsoftenresultfromcollision,losscontrol,
groundingandstructuraldamage,firesorexplosion.
Only from 2011 to 2014 ab
out 4620 cargo ships
involvedinaccidents,of which oiltankersrepresent
about 9% (415 units). In the last decade the total
volume of oil lost to the environment was
approximately 33 000 tonnes. As a result of tankers
incidents increases also the need to carry out the
cargo tra
nsfer between damaged ship and another
one in order to safe cargo (crude oil, petroleum
products, liquefied gas) and to mitigate emission to
theenvironment,calledinnavalterminologytheSTS
(Shiptoship)transfer operation.STS transfer
operation generally involve transshipment between
twoships,thelargecalledSBL(ShiptobeLightered)
and small one called SS (Service Ship) positioned
alongside each other, either while stationary or
underway in order to commence cargo tra
nsfer
(OCIMF/ICS 2005, OCIMF 2009). Usually this
operationiscarriedoutforhuge oil tankersinopen
sea, when ship does not berth in port or jetty,
especially due to draught restrictions or the port
berthing charges. The moti
vation for performing
these operations is a lack of deep water ports and
economic aspects. These types of marine operations
are expected to increase significantly in frequency,
and expand into new geographical areas in the
comingyears.
Before mooring and cargo tra
nsfer start, the
ServiceShiphastoapproachtheShiptobeLightered,
whichmovesonaconstantheadingwithslowspeed
or drifts about zero. For this purpose basically a
collisionavoidancemanoeuvre hasto be carried out
Approach Manoeu
v
re During Emergency Ship-to-Ship
Transfer Operation with Oil Spill
A.Witkowska&R.Śmierzchalski
GdańskUniversityofTechnology,Gdańsk,Poland
P.Wilczyński
GdyniaMaritimeUniversity,Gdynia,Poland
ABSTRACT:OneofthemajoractivitiesduringShiptoShip(STS)transfer operationatseaistosafeapproach
theShiptobeLightered(SBL)whichmovesonaconstantheadingwithslowspeedordrifting.Inthepaper
describedthemanoeuvringproblemforapproachingduringemergencySTStra
nsferoperationwithoilspill.
The approach manoeuvre is considered as a sequence of navigation manoeuvres in specific navigational
environmentwithenvironmentalandoperationalconstraintsaswellasshipdynamicperformance.Additional
constraintsresultsfromSTStransferoperationguideandnavigationpractise.
http://www.transnav.eu
the International Journal
on Marine Navigation
and Safety of Sea Transportation
Volume 11
Number 2
June 2017
DOI:10.12716/1001.11.02.17
332
in order to obtain the required safety distance
betweentwoshipsandtotakesidebysideposition.
The manoeuvringoperations are individually
differentdependingon variation intheenvironment
condition, manoeuvring performance of the
individual ship (Pedersen et al. 2008, Husjord
&Pedersen 2009 , Husjord 2016). During emergency
STS
transfer operation can appear additional
important aspects like ship and cargo condition
(transhipmentfromundamagedside),timelimits(to
ensure fast transhipment) as well as water area
constraints(closetoportarea),avoidancemovingoil
spillorotherrescueunits.
Our objective is to define Approach Manoeuvre
during emergency STS
transfer operation as a
problem of safe trajectory planning for approaching
taking into account weather condition (wind
direction),trafficdensityandstopandspeedcontrol
performance of the vessels involved. Trajectory of
approaching determined on available information
allowstotake propermanoeuvring decisionby ship
operatorusingruddersandpropellersand
tomitigate
oilspilltotheenvironment.
1.2 TheprincipleofastandardApproachManoeuvre
duringSTStransferoperation
The STS transferoperation requires proper
coordination, equipment in according to STS
operation plan and administration approval. The
purpose of the STS transfer operation plan is to
provide a step by
stepdescription of STS procedure
according to guidelines or recommendations from
Iranian Classification Society (ICS), Oil Companies
International Marine Forum (OCIMF) and the
InternationalMaritimeOrganization(IMO).Thisplan
shoulddealwiththefollowingstagesofoperation:
PreApproachPlanning;
ApproachManoeuvre;
Mooring;
CargoTransfer;
Unmooring;
DepartureManoeuvre.
Each stage consists of different procedures to
followandcheckliststocomplete.Astandardwayto
carryoutanSTS transfer operationiswhenthe SBL
maintainaconstantheadingatminimumcontrollable
speed(5knotsorless)ordriftwithwindandcurrents
but SS
approach the first one and berths normally
withitsportsidetothestarboardsideoftheconstant
heading ship (Fig.1). The standard Approach
Manoeuvre is divided into two phases. The initial
phase is basically a collision avoidance manoeuvre
fromcurrentpositionp
otofinalpositionpkinorderto
obtain the required safety distance between Service
ShipandShiptobeLightered.Thesafetydistanceis
called the Distance at Closest Point of Approach
(DCPA) and it is appropriate to the conditions.
DuringthisphaseSSmustapproachthefirstoneona
parallel course and
adjust its velocity to equal SBL.
The second phase which is operation of a ships
alongside takes place after the required safety
distance has been verified. On closer approach, the
manoeuvringshipshouldthenpositionitselfrelative
totheconstantheadingship.Contactismadebythe
manoeuvring ship, reducing the
distance until the
fenderstouch.Subsequentlybothshipsareonparallel
courses with similar velocity and their manifold in
linetominimizeforceofberthingsimultaneouslyon
allfenders.
In the open waters the standard Approach
Manoeuvre begins at distance of 0.5 Nm from the
destinationpointandfinish at
DCPAapproximately
50100m off. The mooring lines startabout 2030m
away from each ship. Normally the manoeuver will
bemadewiththewindandseaahead,howeverlocal
conditionsandknowledgemayindicate an
alternative side. Usually transhipment is completed
after1024hdependingoncargo
qualityandweather
condition.
Throughout any berthing operation the visibility
shouldbegoodenoughforsafemanoeuvring,taking
into account safe navigation and collision avoidance
requirements. This standard Approach Manoeuvre
(Fig.1) is of assistance when ships are under power,
considering normal STS transfer operation. The
proceduresmayvaryfromthis
guidanceaccordingto
circumstances (emergency with oil spill, inshore
operation, limited geographical scope of operation),
dynamical and kinematical ship properties, weather
conditionandtrafficdensity.Ineachuniquesituation
Approach Manoeuvre almost base on knowledge,
experience and assessment of navigational situation
fromnavigators.
Figure1.TheprincipleofastandardApproachManoeuvre
in STS lightering operations (OCIMF/ICS 2005, OCIMF
2009)
The most common incident to occur during STS
operationsisacollisionbetweenthetwoshipswhile
manoeuvring alongside each other or sailing
(Ventikos & Stavrou 2013). Collision between two
ships typically occur for reasons which include:
incorrect approach angle between the manoeuvring
ships;approachingatexcessivespeed; failure ofone
orbothshipstoappreciatemeteorologicalconditions.
To mitigate the risk of incidents, guidelines will be
needed for the navigator of Service Ship, which
include information about reference trajectory for
approaching in meaning of reference way points p
i:
position(x
i,yi )/or(headingi)andvelocityvitotake
333
a proper steering decision by ship operator at each
stageofshipmanoeuvring.
2 OPERATIONASPECTSDURINGEMERGENCY
STSAPPROACHMANOEUVRING
2.1 Accidentscenariowithoiltanker&STSoperationto
mitigateoilspill.
The following example accident scenario with oil
tanker is considered in this paper for trajectory
planning.
Product tankeraftercollision with general
cargo ship lost its ability to manoeuvre and start
drifting NE due to NW’ly wind. Immediate actions
were carried out to reduce oil spill overboard,
arrangedtransfercargofromdamagedtanktoother
compatible tanks and increased heel to port using
ballasttanksto
keepallcracksonbulkheadabovethe
sea water level. Prepare floating cotton barrier to
reduceoilspotinthevicinityofship,startedoilspill
pumpandcollectedoilywatertoslopstanks.Atthe
same time all parties (administration, owner,
charterer, insurer, SAR) were informed accordingly.
Small tanker with
very good manoeuvring
characteristic was designated to emergency STS
operation.
For considered accident with oil tanker two
variants of Approach Manoeuvres are proposed
based on good navigation practice and STS transfer
operation guide (OCIMF/ICS 2005, OCIMF 2009,
Wilczynski 2014). They depend on different
circumstances like wind direction, oil spill area
and
shipactuatorequipment(manoeuvringperformance).
TheexamplesareshowninFigures23.
Figure2. The example trajectory for approaching in STS
transferoperationswith2controlmodes(I,II)‐variantA
Figure3. The example trajectory for approaching in STS
transferoperationswith3controlmodes(I,II,III)‐variantB
Both manoeuvres are from leeward and to the
starboard side of the constant heading ship. They
differonlyinpossibilitytorunDynamicPositioning
control mode (variant B) or without possibility of
runningit(variantA).
2.2 ControlmodesduringemergencySTSprocedure
The possibility of using different control modes
during
STS procedure depends ( among other) on
ship current velocity and actuator equipment. The
Service Ships dedicated for conducting STS transfer
operation are mostly equipped with aft main
propellerusuallyinconjunctionwithrudderandbow
tunnelthruster.Mainpropellerproducethenecessary
surge force needed for transi t and rudder
produce
yawmomentwhichcanbeusedforsteeringcontrol.
Thetunnelthrusterproducesaswayforceandisonly
effectiveatlowspeed.Thissetofthreeactuatorscan
realizeTrajectoryTrackingoperationofApproaching
and then Berthing. Azimuth thrusters can produce
two force components surge and sway in
the
horizontal plane. They are attractive in Dynamic
Positioningsincetheycanproduceforcesindifferent
directions(Fossen,T.2011).
To control the movement of the Service Ship
during STS Approach Manoeuvre a few general
control modes are possible, in order to achieve the
final Distance from SBL, parallel course
and equal
speed(Fig.2).Theyconsistof:
1 Trajectory Tracking (moderate or highspeed
manoeuvring)
2 StoppingManoeuvre(stopship)
3 DynamicPositioning(lowspeedmanoeuvring)
The control modes mention above are classified
accordingtocontrolobjectivesduringSTSApproach
byusingdifferenttypesofavailableactuatorsinclude
propulsionsystem,
thrustersandrudders.
Trajectory Tracking (Tomera 2016): The first
control objective is to minimize a tracking error
betweenadesiredtrajectorygivenbyadesiredtime
varying position and velocity reference signals.
334
DuringSTSoperationtrackingcontrolcanbeusedfor
coursechanging manoeuvres and speedchanging
control separately or simultaneously. The task is
mostly realized at the first phase of Approach
Manoeuvre to assume moderate or high ship speed
(more than 2m/s). At this speed rudder for course
control and main
propeller for speed control (ROT
andruderanglecontrol)areonlyeffective.
Stopping Manoeuvre (ABS, 2006): The second
controlobjectiveisrelatedwithareductionofcurrent
shipvelocityalongtrajectorysegmentsbetweenway
points. The stopping ability of the vessel is judged
using emergency stop manoeuvre or normal stop
menouvre. The emergency stopping test must be
performed starting from the test speed. After the
steadystateisachieved,the“fullastern”commandis
given from the engine control mode on the bridge.
Thetestisconsideredtobecompletedwhentheship
speedisaboutzero.
Duringstop manoeuvrethe
operator shouldstop
itsengineandonlycoursekeepingbyusingrudders
amidships. The test is considered to be completed
whentheshipspeedisdeadonthewater.
Dynamic Positioning (Fossen, 2011, Witkowska
2013). The third control objective consist in
manoeuvringtheshipatlowspeed(lessthan
2m/s).
The only course and position control are associated
withthismode.Atthesespeedshipsteeringiscarried
outbyusingmostlyazimuththrusters,bowthrusters,
sternthrusters,waterjets.Theefficiencyofruddersat
low velocitysignificantly decreases.Dynamic
Positioning mode can be activated at last phase of
approaching(afterspeedreduction)torealizevarious
kindofshipmovementlikelongitudinal,transverse,
rotationarounditsaxisorsidemanoeuvreatcertain
angle.
After Approach Manoeuvre by using I, II or/and
III control modes, the ships should manoeuvres
alongside at the required safety distance (DCPA).
That means both SS
and SBL keep their constant
heading
SS SBL
and constant speed
SS SBL
vv
or drifting about 0. In this condition the Berthing
operation by using tunnel thruster and Mooring
procedurebyusinglinescanstart.
2.3 Stoppingandspeedcontrolcharacteristics
Comprehensive details of the ship stopping and
speed control characteristics are included in the
manoeuvring booklet. This booklet is required to be
on board and available for navigators. Most of the
manoeuvring information in the booklet can be
estimated but some should be obtained from trials.
They contain (among other relevant data)
characteristics of main engine, stopping test results
(emergency and normal) and deceleration
performance. The characteristics of main engine
contain possible engine
order (Full Sea Ahead, Full
Ahead,HalfAhead,SlowAhead,DeadSlowAhead,
Dead Slow Astern, Slow Astern, Half Astern, Full
Astern), propeller revolution, speed, power, pitch
ratio.
Stopping ability is measured by the track reach,
head reach, side reach, time required to speed
reductionandfinalcourse(Fig.4).
Figure4.Definitionusedinstoppingtest.
It covers the following modes of stopping
manoeuvers: from Full Sea Ahead to Full Astern;
fromFullAheadtoFullAstern;fromHalfAheadto
Full Astern; from Slow Ahead to Full Astern; from
Full Sea Ahead to stop engine; from Full Ahead to
stop engine; from Half Ahead to stop
engine; from
SlowAheadtostopengine.
Deceleration performance concern track reach,
headreachandtimerequired.Itcoversthefollowing
modes:fromFullSeaSpeedtoFullAhead;fromFull
Ahead to Half Ahead; from Half Ahead to Slow
Ahead;fromSlowAheadtoDeadSlowAhead.When
the
vessel travels along a straight line with the
original course (autopilot is on) the track reach and
time reach values are taken as the longest travelling
distance and the maximum time to decelerate ship
velocity.
3 TRAJECTORYPLANNINGFORAPPROACHING
The Service Ship trajectory
P
for approaching is
defined as a set of turning points
01
, ,...,
k
pp pP on ship route from current
position (initial point)
0
to the destination (final
point)
k
. The way points
, , , 0,1, ,
iiii
pxyv i k
of desired trajectory
haveposition
,
ii
x
y determinedtoavoidobstacleson
considered area with respect to a top ship speed
, 0,1, ,
i
vi k on each way points. The way
pointsdivide trajectoryintoa set
12
,,,
k
Sss s
of trajectory segments with a lengths
12
,,,
k
Ddd d. The
i
s compose of the path
position sequences between way points on straight
line. The way points components are respectively
reference ship position and speed on each turning
point.
PlanningofthesafetrajectoryduringSTSassumed
that each of trajectory segment
, 1, ,
i
si k ,
between way
, 0, ,
i
p
ik points does not cross
in the area of the environment with the static and
dynamicobstacles.Thechoiceoftopspeedelements
,
i
v
0,1, ,ik at each way points of desired
trajectory depend on set
i
vV
,
0, , , , ,
FA HA SA DSA
Vvvvv where the following
engineordersareconsidered:FullAhead(
FA
v ),Half
Ahead (
H
A
v ), Slow Ahead (
SA
v ), Dead Slow Ahead
(
D
SA
v ).
The designed trajectory satisfies deceleration
conditioniftheshipisableoneachtrajectorysegment
335
1i
s
todecelerateshipvelocityfrom.Itmeansthatfor
a given starting reference speed
i
v at
i
p
it is
possibletoapproachbyshiptheendingone
1ii
vv
at
1i
p
with segment length
1i
d
. The feasibility of
trajectoryischeckedbasedonstopandspeedcontrol
constraints collected in manoeuvring booklet. When
thevesseltravelsinastraightlinealongtheoriginal
course the segment length value can’t be less than
track reach needed for speed deceleration or stop
ship:
11
ii
d track reach

(1)
where
1
i
track reach
isthetravellingdistanceneed
todecelerateshipvelocityfrom
i
v to
1i
v
.
The planning of the last way points
, 2, 1,
i
p
ik k k , 2k depend additionally
on ship manoeuvrability constraints during STS,
results by using variants A or B of Approach
Manoeuvre.
3.1 Waypointsplanning‐variantA
Theinitialwaypoint
0
consistofacurrentposition

00
,
x
y andvelocity
0
v ofServiceShipwhenitstart
Approach Manoeuvre (Fig. 5). The destination point

, ,
kkkk
p
xyv hasaparallelposition

s
sSBL
ll in
asafetydistance(DCPA)frompositionofShiptobe
Lightered and the some velocity
k
vv , to allow
starting manoeuvring alongside. When emergency
STStrajectoryisplanningtheSBLmaintainitscurrent
position

,
x
y constant and speed about zero,
0v . In this case the initial p0 and destination pk
pointsareapproximatelyconstantandchosenbythe
operator or calculated by the simple geometric
relationship:

,
| , ,
kk
kSSSSSBL
xy
p
ll l (2)


2
,
,
0, | | ,
kk
kk
xy
xy
vDCPApp
(3)
where



,
,
| , , | , ,
kk
kkk
xy
xy
p
xy p x y
SS
l straightlinecoversSSdiametricalline,
SBL
l straightlinecoversSBLdiametricalline.
The previous way point
1
k
p
has position
determinedonstraightline
SS
l parallelto
SBL
l .

11
1
,
| ,
kk
kSSSSSBL
xy
p
lll

. (4)
The reference speed
1
k
v
is modelled as
minimum controllable speed
D
SA
v (Dead Slow
Ahead)forsafetymanoeuvringincloseproximity.
1
,
kDSA
vv
(5)
with satisfying feasibility condition of trajectory
segment
k
s :

11
1 2
, ,
| |
kk kk
kk k k
xy xy
d p p track reach

(6)
where
k
track reach is the travelling distance need
todecelerateshipvelocityfrom
D
SA
v toabout0.
The way point
1k
p
is determined on the arc
A
B
L
between the end points A and
B
satisfying
SS
Al
. The arc is a part of a circle
, ,
k
Op AO
witharadius
0.5AO nauticalmilesofcellsand
central angle
0
0, 30
. We also assume that
reference velocity
2kDSA
vv
is predetermine as
minimumcontrollable.

22
2
,
| ,
kk
kABss
xy
p
LAl


(7)
2kDSA
vv
(8)
where
0
, , , 0,30 , 0.5NM
AB k
LOpAO AO

3.2 Waypointsplanning‐variantsB
ThedifferencebetweenvariantsA(Fig.5)andB(Fig.
6) lie only in modelling two way points
,2,1
i
pi k k
. Because of using Dynamic
Positioning control mode, the maximum reference
velocity
1k
v
of approaching doesn’t exceed 1 knots
in the safety area of 0.3 NM [17] from destination
point. The DP system at low speed allow to realize
variouskindofshipmovement,sothepoint
1k
p
is
determined on the larger arc
CD
L with a central
angle
0
0,90
.
1
1 ,
k
vknot
 (9)

11
1
,
|
kk
kCD
xy
p
L

, .
s
s
Cl
(10)
where
0
, , , 0,90 ,
CD k
LOpCO



0.5NM 0.3NMCO
.
The way point
2k
p
is determined on the arc
LAB between the end points
A and
B
satisfying
SS
Al
. The arc is a part of a circle

, ,,
k
Op AO
with a radius
0.5 AO nautical miles of cells and
centralangle
0
0,90
.Weassumethatreference
velocity
2k
v
is predetermineas minimum
controllable (Dead Slow Ahead) for safety
manoeuvring:
2kDSA
vv
, (11)

22
2
,
|
kk
k
xy
p

LAB,
SS
Al
(12)
where
336

0
, , , 0,90 , 0.5NM.
AB k
LOpAO AO


Figure5.Modelingwaypoints‐variantA
Figure6.Modelingwaypoints‐variantB
To satisfy deceleration condition on trajectory
segment
1k
s
a distance
1k
d
can’t be less than a
track reach calculated on stop and low speed
characteristics:

11
12 1 2
, ,
| |
kk kk
kk k
xy xy
dp p


1
k
track reach
(13)
where
1
k
track reach
isthetravellingdistanceneed
toreduction
2k
v
to
1k
v
1knot.
Additional constraints on way points depend on
winddirection(sideofmanoeuvreifitpossiblefrom
leeward)and emergency condition(sideof
manoeuvreapproachfromundamagedside)
4 CONCLUSIONS
The paper formulate the problem of Approach
ManoeuvreduringemergencySTStransferoperation
withoilspillasaproblemof
trajectoryplanning for
approaching. The trajectory is considered as a
sequence of way points with reference position and
velocity and straight line segments between them.
Thewaypointplanningprocessresultsfromtransfer
operationguide,shipoperationconstraintsandwith
respect to additional constraints depended on ship
speedandstopping
meneuverperformance.
The presented in above way trajectory planning
issue can be consider as an example of classical
avoiding collisions at sea. It can be reduced as a
multicriteria, nonlinear optimization problem with
navigational time, safety and economy criteria with
navigationalconstraints:
stationaryobstacles (land,islands, shallowwater,
restricted
area)
dynamical obstacles (SBL ship, other ships,
modeling of the prediction of the oil spill area
(Łazugaetal.2012)
modelingofshipsandobstaclesbydomains
ships and obstacles domains position, course,
speed.
weathercondition(winddirection)
stoppingandspeedcontrolcharacteristics
Several
solutionscanbeusedtosolvetheproblem
of trajectory planning for approaching defined as
optimization task. One of them contain Genetic or
Evolutionary Algorithm (Kuczkowski &
Smierzchalski 2014), Particle Swarm Algorithm
(Lazarowska 2015), Simulated Annealing (SA). The
results of using Evolutionary Algorithm with taking
into account speed deceleration and stopping
characteristics for trajectory planning during
emergency STS transfer operation is the aim of the
followingstageofresearch.
ACKNOWLEDGEMENT
Thepaperpresentstheresultsdevelopedinthescope
oftheHAZARDprojecttitled“MitigatingtheEffects
of Emergencies in Baltic Sea Region Ports” that has
receivedfundingfromtheInterreg
BalticSeaRegion
Programme 20142020 under grant agreement No
#R023.https://blogit.utu.fi/hazard/
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