438
POSistheprobabilityoflocatingthesearchobject.
Itis the true measure of effectiveness. Theability to
findanobjectdependsonhavingasensorcapableof
detecting the object and placing this sensor close
enoughtothesearchobjectthatitsdetectionwouldbe
probable.Thisvalue
iscalculatedfromthefollowing
relation:
POS POC x POD (2)
where, POC=Probability of Containment,
POD=ProbabilityofDetection.
Probability of containment (POC) – expresses the
probability that the searched object is within the
search area. The probability area is defined as the
smallestareathatcontainsallpossibleobjectlocations
(inthiscasePOC=100%).Inmanysituations,the
area
issolargethatitcannotbesearchedbyavailableSRU.
Ithappensoftenthatsomesub‐areasaremorelikely
tocontainthesearchobjectthanothers.Therefore,the
areacanbedividedintosmallersectors,forwhichthe
SRUs would be deployed. The POC measures the
probability of
achance to detect an object if it is
actually located within the area. The exact way to
determine the POC is described in the IAMSAR
Manual vol. II“Mission Co‐ordination” and will not
bediscussedindetailinthispaper.
Probability of Detection (POD) is the probability
thatthesearchedobjectwillbefound,assumingthat
in fact it is in the search area. POD dependent on
coverage coefficient, detector sensor, search
conditions and accuracy with which rescue units
navigatethedesignatedsearchpattern.Thecoverage
factor(C)comparestheamountofsearchingthatcan
bedoneto
thesizeofnecessarysearch.Thecoverage
factorcanbeexpressedastheratioofsearcheffort(Z)
to the size of the search area (A), or as the ratio of
sweepwidth(W)andthetrackspacing(S).Coverage
factoristobecalculatedasfollows:C=Z/AorC=W/S.
Searcheffort(Z) of a SRU representthearea that
can be effectively searched by particular unit. The
search effort is computed as the product of search
speed (V), search endurance (T), and sweep width
(W)Z=V*T*W.Sweepwidthdefineshowwideisthe
scanningstripforaSRU.It’sa
measureoftheability
to detect a search object. It takes into account
environmentalconditions(visibility,seastate),sizeof
theobjectandtheoperatorfatigue.Itisprovidedasa
guideforsettingthetrackspacing.Thetrackspacing
is the distance between the centres of adjacent SRU
paths.
Atrackspacingthatislessorequaltoone‐half
the corrected sweep width results in POD of 100%.
Thegreaterthesearcheffortcomparedto the search
area, the higher the coverage ratio (analogically
sweepwidthtotrackspacing).
Selection of SRU for a given task bases on
effectiveness
indicators. The SRU perform different
potential effectiveness depending on the speed,
observation altitude, seaworthiness, range and
detectionequipment.
2 WIGCRAFT
In recent years, the development of technology for
vehicle moving in the ground effect has been
resumed.TheWIGCraftmeansWing‐In‐Ground‐Effect
Craft.Thegroundeffect
isaphysicalphenomenonof
creationanaircushionbetweentheflyingvehicleand
the surface over which it moves. As a result air
pressuredifferencebetweentheareaunderthewings
andoverthewingsappears,andanadditionallifting
forcedirectedupwardsiscreated.Consequently,the
craftachieves
relativelyhighspeedwithverylowfuel
consumption.Birds use this physical principle when
overcomeverylargedistancesabovethesurfaceofa
lakewithoutmovingthewings.Thecraftoperatingin
ground effect flies at a low altitude, which is equal
about 1/3 of the span of its wings, usually
a few
meters.ThemainconstraintsfortheoperationofWIG
craft are hydro‐meteorological conditions. A large
wavescan hinder ordestabilizea flightof a craftin
the ground effect, since it needs a flat surface. The
WIGCraftsareclassifiedunderashipinaccordance
to the
IMO (International Maritime Organization).
WIG units are cheaper to build and maintain than
traditionalairborneunits,andcrewtrainingcostsare
alsolower(comparabletomarinestafftrainingcosts).
WIG units do not also require any special aviation
infrastructureastheyarestationingattheports.The
WISECraft(Wing‐In
‐Surface‐EffectCraft)orEkranoplan
arethe common namesfor WIG Crafts. (Górtowska,
2012)
Examples of modern WIG crafts used for search
and rescue tasks at sea are: Rescue Unit Aron‐7
(Figure1)orMulti‐TaskMarineEkranoplanES‐108.
Aron‐7isaIMOtypeB*WIGcraft
forsearchtasks
(*type B means that in addition to a flight in the
groundeffect,theunithastheoptionofleavingitand
elevates). The craft has been registered by
GermanischerLloyd.
The craft aviates within an altitude of 5 m in
groundeffect,atamaximumspeed
of200km/h(108
knots). The cruising speed is 120‐150 km/h (65‐81
knots). The vehicle has a length of 10 meters,
wingspan12 meters, height 2.9meters. The range of
the craft is 800 km (432Nm). The number of
passengersis5(two‐personcrew).
Figure1. WIG Craft Aron‐7 during take‐off phase. Source:
www.cnsamt.com
A motor is placed at the top of the cabin. The
wingsareintheshapeofanelongatedtrapezoid,and
theballastsaremountedtothemainpartofthehull.