Two-Part Towing System
Two-Part Towing System
Two-Part Towing System
www.elsevier.com/locate/oceaneng
Abstract
1. Introduction
Underwater towed systems are fundamental tools for many marine applications
which include naval defense, seabed mapping and ocean environmental measure-
ments. These systems can be as simple as a single cable with its towed vehicle, or
they may be composed of multiple towed cables and multiple towed bodies.
* Corresponding author.
0029-8018/00/$ - see front matter 1999 Elsevier Science Ltd. All rights reserved.
PII: S 0 0 2 9 - 8 0 1 8 ( 9 9 ) 0 0 0 0 6 - 2
456 J. Wu, A.T. Chwang / Ocean Engineering 27 (2000) 455–472
The system described in this paper consists of primary, secondary and depressor
cables, and the towed vehicle and the depressor are attached to the end of secondary
and depressor cables respectively (Fig. 1). The primary cable and depressor cable
are negative buoyant, while the towed vehicle and the secondary cable are neu-
trally buoyant.
Three different coordinate systems are used in the derivation of equations, i.e. the
fixed inertial coordinate system (X,Y,Z) and local coordinate systems for cables (t,n,b)
and for the towed vehicle (x,y,z) as shown in Fig. 1. The governing equations for
cables are given first, then three cables are modeled separately and interfaced
dynamically at the conjunction. The speed of the towing ship on the water surface
and dynamic equations of the towed vehicle and the depressor are taken as boundary
conditions for governing equations of cables. For results presented in this paper,
computations start from a steady state solution which is taken as the initial condition
for the whole system.
458 J. Wu, A.T. Chwang / Ocean Engineering 27 (2000) 455–472
The cable is treated as a long, thin, flexible circular cylinder. It is assumed that
the dynamics of a cable are determined by gravity, hydrodynamic loading and inertial
forces, no bending or torsional stiffness is taken into account in this study.
The equations are written in orthogonal coordinates (t, n, b) local to each point
of the cable. The orthogonal coordinates (i, j, k) represent the fixed inertial frame,
i, j being in the horizontal plane and k pointing downward. The origins of systems
(i, j, k) and (t, n, b) are coincident. The orientation of the local frame is so chosen
that t is tangent to the cable in the direction of increasing unstretched cable length
coordinate s, b is in the plane of i and j, t and n lie in a vertical plane. At any point
of a cable the two frames (i, j, k) and (t, n, b) are related by
(t,n,b) ⫽ (i,j,k)[D], (1)
where
冤 冥
coscos ⫺ cossin sin
[D] ⫽ sincos ⫺ sinsin ⫺ cos .
sin cos 0
Eq. (1) represents a rotation through angle about the k axis to bring i axis into
the plane of t and n, rotation about the new i axis through /2 to bring k into
coincidence with b, and rotation about b through to bring i and j into coincidence
with t and n. The relative position of two coordinate systems is shown in Fig. 2.
Similar to Ablow and Schechter (1983), at any point of cables, the governing
equation can be written as
MY⬘ ⫽ NẎ ⫹ Q,
J. Wu, A.T. Chwang / Ocean Engineering 27 (2000) 455–472 459
∂Y ∂Y
Y ⫽ (T,t,n,b,,)T, Y⬘ ⫽ , Ẏ ⫽ ,
∂s ∂t
1 0 0 0 0 0
M⫽
0 1 0 0
0 0 1 0
bcos
⫺ bsin
⫺ n
t
, (2)
0 0 0 1 ⫺ tcos ⫹ nsin 0
0 0 0 0 ⫺ Tcos 0
0 0 0 0 0 T
⫺ mevt
m 0 0 m1bcos ⫺ m1n
1 ⫹ eT
e 0 0 0 0 0
0 0 0 0 0 1 ⫹ eT
N⫽ 0 0 0 0 ⫺ (1 ⫹ eT)cos 0 ,
em1b
⫺ 0 0 m1 m1nsin ⫺ mtcos 0
1 ⫹ eT
em1n
⫺ 0 m1 0 ⫺ m1bsin m t
1 ⫹ eT
⫺ w sin ⫹ (1 ⫹ eT)1/2 21 dCtt兩t兩
Q⫽
0
0
,
0
1
2 dCn(2n ⫹ 2b)1/2b(1 ⫹ eT)1/2
⫺ w cos ⫹ 1
2 dCn(1 ⫹ eT)1/2n(2n ⫹ 2b)1/2
460 J. Wu, A.T. Chwang / Ocean Engineering 27 (2000) 455–472
where T denotes the tension force of the cable, t, n and b are the velocity compo-
nents along the t, n and b directions respectively, m is the mass per unit length of
cable, m1 is equal to m ⫹ A ( being the density of water and A the cross-sectional
area of the unstretched cable), e is equal to 1/EA (E being the Young’s modulus of
cable), w is the submerged weight per unit length of a cable, and d is the cable diam-
eter.
The velocity components of three cables at the conjunction point must be identical
and resultant forces of three cables at that point must be zero. Therefore
VPN ⫽ VD0 ⫽ VS0, (3a)
⌺T ⫽ 0, (4a)
or
冤冥 冤冥 冤冥
t t t
[D]PN n ⫽ [D]D0 n ⫽ [D]S0 n , (3b)
b PN b D0 b S0
冤冥 冤冥 冤冥
Tt Tt Tt
[D]PN 0 ⫹ [D]D0 0 ⫹ [D]S0 0 ⫽ 0, (4b)
0 PN 0 D0 0 S0
where subscripts P, D, and S denote the primary, depressor and secondary cables
respectively, and subscripts 0 and N denote the first and last node, the directions of
the cables are shown in Fig. 1.
The relation between the towing ship velocity and the towing point velocity of
the primary cable is
[t,n,b]P0 ⫽ [Sx,Sy,Sz][D]P0, (5)
where Sx, Sy and Sz are the velocity components of the towing ship in inertial coordi-
nates.
In this paper the depressor is assumed to be a weighted ball. Therefore, at the end
of the depressor cable (node DN) the boundary condition is
TDN ⫽ ⫺ 1
2 CDDSD兩VDN兩VDN ⫺ (C1⌬ ⫹ m0)V̇DN ⫹ w0k, (6)
where CDD is the drag coefficient of depressor, SD the projected area of depressor,
C1 the added-mass coefficient of depressor, ⌬ the volume of depressor, m0 the mass
of depressor and w0 the submerged weight of depressor. The values of T, and
at node DN are determined from Eq. (6).
The velocity coupling relation between the end of the secondary cable (node SN)
and the towing point of a towed vehicle is
J. Wu, A.T. Chwang / Ocean Engineering 27 (2000) 455–472 461
the towed vehicle in the vehicle-fixed coordinate, rT ⫽ (xT, yT, zT) is the towing point
coordinates in the vehicle-fixed frame, VSN is expressed in local coordinates of
cable and
[E]
冤 冥
coscos cossin ⫺ sin
⫽ ⫺ sincos ⫹ sinsincos coscos ⫹ sinsinsin sincos ,
sinsin ⫹ coscossin ⫺ sincos ⫹ cossinsin coscos
where , and are the pitch, roll and yaw angles of the towed vehicle.
The six-degrees-of-freedom equations of motion for a towed vehicle in surge,
sway, heave, roll, pitch, and yaw can be written as (Gertler and Hagen, 1967)
m[u̇ ⫺ r ⫹ wq ⫺ xG(q2 ⫹ r2) ⫹ yG(pq ⫺ ṙ) ⫹ zG(pr ⫹ q̇)] ⫽ XH (8)
⫹ XW ⫹ XC ⫹ XT,
m[˙ ⫹ ur ⫺ wp ⫹ xG(pq ⫹ ṙ) ⫺ yG(p2 ⫹ r2) ⫹ zG(qr ⫺ ṗ)] ⫽ YH (9)
⫹ YW ⫹ YC ⫹ YT,
m[ẇ ⫺ uq ⫹ vp ⫹ xG(pr ⫺ q̇) ⫹ yG(qr ⫹ ṗ) ⫺ zG(p2 ⫹ q2)] ⫽ ZH (10)
⫹ ZW ⫹ ZC ⫹ ZT,
Ixṗ ⫹ (Iz ⫺ Iy)qr ⫹ Ixy(pr ⫺ q̇) ⫺ Iyz(q2 ⫺ r2) ⫺ Ixz(pq ⫹ ṙ) (11)
⫹ m[yG(ẇ ⫺ uq ⫹ vp) ⫺ zG(v̇ ⫹ ur ⫺ wp)] ⫽ KH ⫹ KW ⫹ KC ⫹ KT,
Iyq̇ ⫹ (Ix ⫺ Iz)pr ⫺ Ixy(qr ⫹ ṗ) ⫹ Iyz(pq ⫺ ṙ) ⫹ Ixz(p2 ⫺ r2)
⫺ m[xG(ẇ ⫺ uq ⫹ vp) ⫺ zG(u̇ ⫺ vr ⫹ wq)] ⫽ MH ⫹ MW ⫹ MC (12)
⫹ MT,
Izṙ ⫹ (Iy ⫺ Ix)pq ⫺ Ixy(p2 ⫺ q2) ⫺ Iyz(pr ⫹ q̇) ⫹ Ixz(qr ⫺ ṗ) (13)
⫹ m[xG(˙ ⫹ ur ⫺ wp) ⫺ yG(u̇ ⫺ vr ⫹ wq)] ⫽ NH ⫹ NW ⫹ NC ⫹ NT,
where the left-hand sides represent inertial forces and moments and the right-hand
sides denote external forces on the towed vehicle. Subscript H reflects hydrodynamic
contributions, W buoyant and weight effects, C forces arising from control surfaces
(control wing, flap etc.) and T towing forces. The symbols in the equations are based
on the standard notation.
The towed vehicle being investigated in this paper is assumed to be a circular
cylinder with symmetry about its center of uniform mass located at the mid point
of the vehicle. There is no control surfaces in such a type of towed vehicle. Thus
control forces do not exist. The hydrodynamic forces acting on the towed vehicle
are given by
462 J. Wu, A.T. Chwang / Ocean Engineering 27 (2000) 455–472
The towing forces and moments on the towed vehicle in local coordinates of the
vehicle are
冤冥
XT
FT ⫽ YT ⫽ ⫺ [E][D]SNTSN, (27)
ZT
[KT,MT,NT] ⫽ rT ⫻ FT. (28)
To complete the hydrodynamic model of the towed system, the expression for the
rates of change of Euler angles for the towed vehicle is
˙ ⫽ p ⫹ q sintan ⫹ r costan, (29)
˙ ⫽ q cos ⫺ r sin, (30)
J. Wu, A.T. Chwang / Ocean Engineering 27 (2000) 455–472 463
sin cos
˙ ⫽ q ⫹r . (31)
cos cos
For results presented in this paper, constant velocity of the towing ship Vts is
assumed to be the initial state, that is, Vts ⫽ ⫺ V0i and
∂
t ⫽ ⫺ V0cos, n ⫽ V0sin, b ⫽ 0, ⫽ 0, ⫽ 0. (32)
∂t
The governing equation of cables (Eq. (2)) with the conditions described in Section
2.2 determines the towed system parameters completely. In this study the partial
differential Eq. (2) is approximated by a finite difference equation centered in time
and in space. Three cables are divided into a series of segments of length ⌬Sj and
time is divided into a series of time steps ⌬t. The node numbers in three cables are
0 苲 NP, 0 苲 ND, 0 苲 NS respectively, 6 node variables Yj ⫽ (T, t, n, b, ,)Tj
(j⫽0 苲 N, N ⫽ NP, ND or NS) are included at each node of cables. The finite differ-
ence approximation of Eq. (2) is written at mid point of each cable segment
(Burgess, 1991),
⫹ 1 ⫺ Yj
Yij ⫹ Yij ⫹ 1 ⫺ Yij
1 i⫹1
⫹ 1 ⫹ Mj
[Mij ⫹ ⫹ [Mij ⫹ 1 ⫹ Mij ] ⫽ [Nij ⫹
1 i⫹1 1
] ⫹1
⌬Sj ⌬Sj
⫹ 1 ⫺ Yj ⫹ 1
Yij ⫹ Yij ⫹ 1 ⫺ Yij
1 i
⫹ Nij ⫹ 1] ⫹ [Nij ⫹ 1 ⫹ Nij ] ⫹ 1 ⫹ Qj
⫹ Qij ⫹ 1 i⫹1
(33)
⌬t ⌬t
⫹ Qij ⫹ 1 ⫹ Qij ,
where superscript i denotes i-th time step.
The finite difference equations include all node variables in three cables, there are
6(NP ⫹ ND ⫹ NS ⫹ 3) unknown variables Yj of all three cables with 6(NP ⫹ ND ⫹
NS) finite difference equations in Eq. (33). The rest 18 scalar equations are provided
by Eq. (3a), (3b), (4a), (4b)–(7) in finite difference form. However, Eq. (7) introduces
9 new variables, that is, 3 translational velocity components (u, v, w), 3 angular
velocity components (p, q, r) and 3 Euler angles (, , ) of the towed vehicle.
Therefore, 9 more equations are needed to solve the problem. These 9 equations are
given by Eqs. (8)–(13) and Eqs. (29)–(31).
Let g(Y) ⫽ 0 be the [6(NP ⫹ ND ⫹ NS ⫹ 3) ⫹ 9] nonlinear algebraic equations
as established above, and variables Y are ordered as
Y ⫽ 兵YPj,YDj,YSj,(u,v,w,p,q,r),(,,)其T, (34)
P D S
where Y , Y and Y are all node variables in the primary, depressor and secondary
j j j
cables ordered from the first to the last node. The components of g are arranged
as follows:
464 J. Wu, A.T. Chwang / Ocean Engineering 27 (2000) 455–472
Fig. 3. The block structure of the Jacobian. The shaded submatrices indicate potential fill-in outside
block tridiagonal in the same columns as S01.
J. Wu, A.T. Chwang / Ocean Engineering 27 (2000) 455–472 465
derivatives of Eq. (3a), (3b), (4a) and (4b) with respect to the variables at node S0
of the secondary cable.
The Gaussian elimination with partial pivoting is applied to solve Eq. (36). In this
work, the Jacobian J is stored in the matrices as shown in Fig. 4. The block tridia-
gonal submatrices are stored in M and in EN, and submatrix S01 together with out-
side block tridiagonal potential fill-in submatrices (shaded submatrices as shown in
Fig. 3) which are located in the same columns as S01 are stored in EX. Numerical
manipulation to solve Eq. (36) is carried out in these matrices, only nonzero submatr-
ices of the Jacobian are dealt with in this algorithm. The choice of pivotal element
and elimination of nonzero elements below the main diagonal are conducted in the
first column of matrix M or EN. When the first element is eliminated in a row, all
remaining elements in that row move up one entry and set the last entry (column
12 in M or column 15 in EN) in that row equal to zero. Same row exchange and
row elimination are conducted in the matrix EX when the numerical operations deal
with the outside block tridiagonal submatrices. Backsubstitution is carried out after
the elimination process, and finally Eq. (36) can be solved.
The computer program based on the above established model gives the three-
dimensional shape of the system, the tension and velocity components along the
Fig. 4. The storage of the Jacobian. The dashed line submatrix in EN indicates the transfer matrix
between M and EN.
466 J. Wu, A.T. Chwang / Ocean Engineering 27 (2000) 455–472
three cable nodes and also the velocities and Euler angles of the towed vehicle at
each time step. The direction of towing path and the towing point speed may be
changed at any time. Thus the model can easily be used to predict the system
response during different maneuvers. In this section numerical simulations are given
to discuss the hydrodynamic characteristics of this kind of underwater towed system.
The particulars of cables, depressor and the towed vehicle used in the investi-
gations are
Depressor: diameter ⫽ 0.85 m, weight in water ⫽ 2000 kg,
Towed vehicle: D ⫽ 0.3 m, L ⫽ 2.0 m, yT ⫽ zT ⫽ 0, xT ⫽ ⫺ L/2,
Cable: d ⫽ 0.02 m, Ct ⫽ 0.02, Cn ⫽ 2.0, SP ⫽ 300 m, and mP ⫽ 2.7 kg/m, SD
⫽ 6 m, and mD ⫽ 2.7 kg/m, SS ⫽ 20 m, and mS ⫽ A kg/m,
where L is the length of towed vehicle, Ct and Cn are tangential and normal drag
coefficients of cables and SP, SD and SS are the lengths of three cables.
冋冉
⫹ 0rhcos kV0 ⫹
2
T0 冊 册
t ⫹ h k,
where k is the wave number, s and h are phase differences of surge and heave,
the values used in Eq. (37) are given in Table 1.
Fig. 5 shows the time histories of vertical displacements of the towed vehicle and
the depressor. It can be seen that the amplitude of the towed vehicle is about one
sixth of that of the depressor, which indicates that the two-part tow method does
reduce the heaving response of the towed vehicle. In Fig. 5 the low frequency oscil-
Table 1
The values used in the numerical simulation
Fig. 5. Time histories of vertical displacements of the towed vehicle and the depressor.
lations of the towed vehicle and the depressor are caused by the sinusoidal movement
of the towing ship in the horizontal plane.
The two-part tow method basically has no influence on the sway or surge behavior
of the towed vehicle. The time histories of the towed vehicle and the depressor are
similar in surge or sway (Figs. 6 and 7). In Fig. 8 the roll, pitch and yaw angles of
a towed vehicle during the above maneuver are shown. It can be seen from Fig. 8
that even though there is no other control measure, the pitching angle of the towed
vehicle remains very small (兩兩 ⱕ 1.0°), which is within the permitted limit of most
towed vehicle’s requirements. Fig. 9 shows time histories of cable tensions at three
cable ends (nodes P0, DN and SN). It is obvious that the maximum tension occurs
at node P0. The amplitudes of tension vary with different cable ends, the greater the
mean value of tension, the greater the amplitude.
Fig. 7. Time histories of the towed vehicle and the depressor in sway.
Fig. 8. The roll, pitch and yaw angles of the towed vehicle.
In the above numerical simulation, the nodes on the cables are equally spaced.
The discrete segment numbers of the primary, depressor and secondary cables are
30, 3 and 5 respectively. The time steps are held fixed at 0.3 sec in the simulation
and the number of iterations needed for convergence at each time step is about 4.
The selection of the time step in the example is based on the nature of the high
frequency oscillation of the towing point. For low frequency maneuvers such as a
towing ship traveling in still water plane, the time step can be taken as large as 20
to 30 sec with no numerical instability.
J. Wu, A.T. Chwang / Ocean Engineering 27 (2000) 455–472 469
Fig. 10. Heaving ratio between the towed vehicle and the depressor versus the encountering frequency.
470 J. Wu, A.T. Chwang / Ocean Engineering 27 (2000) 455–472
Fig. 11. Heaving ratio between the towed vehicle and the depressor versus the secondary cable length.
(Fig. 11). In order to maintain a towed vehicle at a constant water depth, the length
of the primary cable in a two-part underwater towed system has to be changed under
different towing speeds. Fig. 12 shows the relationship between the towing speed
and the length of primary cable for the towed system as described in this section
when the towed vehicle is kept at 86.3 m water depth. Fig. 13 demonstrates the
heaving responses of the towed vehicle and the depressor versus the towing speed
on the condition that the towed vehicle is kept at about 86.3 m mean value of water
depth under the towing conditions as in Section 4.1. It is found that although the
heaving response of the depressor varies greatly with different towing speed, the
heaving amplitude of the towed vehicle remains very stable and its value is about
0.1 m. The lower the towing speed, the smaller the heaving ratio.
Fig. 12. Relationship between the primary cable length and the towing speed (the depth of the towed
vehicle is fixed at 86.3 m).
J. Wu, A.T. Chwang / Ocean Engineering 27 (2000) 455–472 471
Fig. 13. Heaving responses of the towed vehicle and the depressor versus the towing speed.
Fig. 14 illustrates the time histories of the towed vehicle and the depressor in
heaving under the same towing conditions as in Fig. 5 except that the incident wave
propagates in the negative X direction. Comparing Fig. 14 with Fig. 5 it can be found
that the heaving patterns in two towing conditions are different. The heaving ampli-
tude of the towed vehicle in Fig. 14 is about 2.5 times than that in Fig. 5. The reason
for the difference is that the encountering frequencies of the towing ship in two
towing conditions are different, the former is 0.35 sec (following sea towing) and
the latter is 1.75 sec (head sea towing). According to the observation of Fig. 10, it
is expected that the heaving response of the towed vehicle in a head sea towing will
be smaller than that in a following sea towing.
Fig. 14. Time histories of the vertical displacements of the towed vehicle and the depressor (following
sea towing).
472 J. Wu, A.T. Chwang / Ocean Engineering 27 (2000) 455–472
5. Conclusions
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