2. QUATERNION SHIP DOMAIN (QSD)

The definition of ship domains (Goodwin, Reference Goodwin1975) implies that ship domains are qualitative and quantitative models incorporated with both objective and subjective characteristics. However, most previous ship domain models pursue qualitative investigations; in addition, the subjective ship domains that navigators preserve are usually distinct, with objective models that corresponding vessels should hold. Fortunately, Wang (Wang, Reference Wang2010) proposed a novel Quaternion Ship Domain (QSD) which aims to develop a systematic and analytical approach to a unified framework for modelling ship domains. Unlike the previous circle, ellipsoid and polygon ship domains, the QSD model is characterized by the scale quaternion Q = {R _fore, R_aft, R_port, R_starb} and the shape parameter k, whereby Q indicates the radii of fore, aft, starboard and port directions of own ship. The formulae could be rewritten as follows:

(1)$$QSD_k = \{ (x,y)|f_k (x,y;Q) \leqslant 1,Q = \{ R_{\,fore}, R_{aft}, R_{starb}, R_{\,port} \}, k \geqslant 1\} $$

(2)$$\eqalign{f_k (x,y;Q) = & \left( {\displaystyle{{2x} \over {(1 + {\mathop{\rm sgn}} (x))R_{fore} - (1 - {\mathop{\rm sgn}} (x))R_{aft}}}} \right)^k \cr & + \left( {\displaystyle{{2y} \over {(1 + {\mathop{\rm sgn}} (y))R_{starb} - (1 - {\mathop{\rm sgn}} (y))R_{port}}}} \right)^k} $$

where sgn(.) is a sign function defined in Equation (3):

(3)$${\mathop{\rm sgn}} x = \left\{ {\matrix{ {1,} & {x \geqslant 0} \cr { - 1,} & {x \lt 0} \cr}} \right.$$

In addition, Wang (Wang, Reference Wang2010) determined the Q and k parameters, by considering parts of the dynamic and stationary affecting factors via following nonlinearities:

(4)$$\left\{ \matrix{R_{\,fore} = (1 + 1.34\sqrt {k_{AD}^2 + (k_{DT} /2)^2} )L \hfill \cr R_{aft} = (1 + 0.67\sqrt {k_{AD}^2 + (k_{DT} /2)^2} )L \hfill \cr R_{starb} = (0.2 + k_{DT} )L \hfill \cr R_{\,port} = (0.2 + 0.75k_{DT} )L \hfill} \right.$$

where:

• L is the own ship length.

• k _AD and k _DT represent gains of the advance A _D and the tactical diameter D _T respectively, and can be calculated as follows:

  (5)$$\left\{ \matrix{k_{AD} = A_D /L = 10^{0{\cdot}3591\lg V_{own} + 0{\cdot}0952} \hfill \cr k_{DT} = D_T /L = 10^{0{\cdot}5441\lg V_{own} - 0{\cdot}0795} \hfill} \right.$$
  where V _own is the own ship speed represented in knots.

3. DYNAMIC QUATERNION SHIP DOMAIN (DQSD)

Actually, the scale and shape parameters of the QSD model could be considered as quantitative and qualitative identifications, respectively. Varieties of affecting factors could be efficiently incorporated into this model framework to determine quantitative and qualitative characteristics simultaneously. As a consequence, the subjective and objective features could be merged into a unified model. However, so far, effective identification methods for scale and shape parameters have not been presented to sufficiently build the nonlinear relationship between inputs (i.e., including human, ship and environment factors), and outputs (i.e., ship domain parameters). To be specific, ship domain parameters Q and k should be carefully characterized by human factors, ship manoeuvrability and traffic circumstance, respectively. In order to implement the complete QSD model by considering the abovementioned factors, the whole ship domain termed Dynamic Quaternion Ship Domain (DQSD) could be described as follows:

(6)$$DQSD(t) = f\,(C({\bf \Omega} (t)){\bf Q}({\bf \Theta} (t)),k({\bf \Xi} (t)))$$

where:

• The nonlinear function f(.) defines the DQSD boundary given by Equation (2).

• C(.) is the scalability function evaluating the traffic circumstance.

• Q(.) is quaternion scale vector function, i.e. Q(Θ(t)) = [R _fore(Θ(t)),R _aft(Θ(t)),R _port(Θ(t)),R _starb(Θ(t))]^T, of ship manoeuvrability.

• C(.)Q(.) denotes the scalable quaternion vector.

• k(.) is the shape function dependent on ship navigator's states.

• Ω(t), Θ(t) and Ξ(t) are time-varying environment, ship manoeuvrability and human state vectors including corresponding variables, respectively.

3.1. The Ship Submodel

In order to identify ship factors affecting the DQSD model, we first establish the ship manoeuvrability prediction model by incorporating ship motion models. To be specific, the MMG ship motion model is used to build the second order response manoeuvre model for ship manoeuvrability predictions since the K and T parameters in a Nomoto-type model are directly related to the ability of course changing and keeping. In this case, the ship submodel of DQSD model would be reasonably generated on the basis of ship manoeuvrability.

The MMG ship motion model could be described as follows:

(7)$$\left\{ \matrix{(m + m_x )\dot u - (m + m_y )vr = X_H + X_P + X_R \hfill \cr (m + m_y )\dot v + (m + m_x )ur = Y_H + Y_P + Y_R \hfill \cr (I_{zz} + J_{zz} )\dot r = N_H + N_P + N_R \hfill} \right.$$

where:

• m and I _zz are mass and moment of inertia of the ship, respectively.

• m _x, m_y and J _zz denote added mass in the x- and y-directions and added moment of inertia about z-axis, respectively.

• X, Y and N denote surge forces, sway forces and yaw moments, respectively, due to hydrodynamics, propeller and rudder denoted by subscripts H, P and R.

• u and v are the velocities along X (towards forward) and Y axes (towards starboard) respectively.

• r is the yaw rate.

Apply linearization operation to Equation (7) and omit the high order terms, this becomes:

(8)$$\left\{ {\matrix{ {(m + m_x )\Delta \dot u - (m + m_y )vr = X_u \Delta u} \hfill \cr {(m + m_y )\dot v + (m + m_x )u_0 r = Y_v v + Y_r r + Y_\delta \delta} \hfill \cr {(I_{zz} + J_{zz} )\dot r = N_v v + N_r r + N_\delta \delta} \hfill \cr}} \right.$$

Without loss of generality, assume that the forward speed u keeps constant. Applying Laplace transformation and inverse operation, we obtain the second order response model as follows:

(9)$$\left\{ {\matrix{ {T_1 T_2 \ddot r + (T_1 + T_2 )\dot r + r = K(\delta + T_3 \dot \delta )} \hfill \cr {T_1 T_2 \ddot v + (T_1 + T_2 )\dot v + v = K_v (\delta + T_{3v} \dot \delta )} \hfill \cr}} \right.$$

where the corresponding non-dimensional hydrodynamics derivatives could be determined by the following equations:

(10)$$\left\{ \matrix{T_1 T_2 = \left( {\displaystyle{L \over V}} \right)^2 \displaystyle{{(m' + m'_y )(I'_{zz} + J'_{zz} )} \over {C'}} \hfill \cr T_1 + T_2 = \left( {\displaystyle{L \over V}} \right)\displaystyle{{ - (m' + m'_y )N'_r - (I'_{zz} + J'_{zz} )Y'_v} \over {C'}} \hfill \cr K = \left( {\displaystyle{V \over L}} \right)\displaystyle{{N'_v Y'_\delta - N'_\delta Y'_v} \over {C'}} \hfill \cr T_3 = \left( {\displaystyle{L \over V}} \right)\displaystyle{{(m' + m'_y )N'_\delta} \over {N'_v Y'_\delta - N'_\delta Y'_v}} \hfill \cr K_v = \left( {\displaystyle{V \over L}} \right)\displaystyle{{N'_r Y'_\delta - (Y'_r - (m' + m'_x ))} \over {C'}} \hfill \cr T_{3v} = \left( {\displaystyle{L \over V}} \right)\displaystyle{{Y'_\delta (I'_{zz} + J'_{zz} )} \over {N'_r Y'_\delta - (Y'_r - (m' + m'_x ))}} \hfill \cr C' = N'_r Y'_v - N'_v (Y'_r - (m' + m'_x )) \hfill} \right.$$

where:

• L denotes ship length.

• V = (u ² + v ²)^0·5 is ship speed.

Other coefficients are non-dimensional hydrodynamics derivatives which can be derived from ship dynamic and stationary parameters Θ(t) = [Θ_Sta, Θ_Dyn(t)]^T, where stationary parameter vector Θ_Sta mainly includes ship length L, width B, block coefficient C _b, draft d, displacement ∇, rudder area A _R, height of rudder H _R and propeller diameter D _P, etc., while dynamic parameter vector Θ_Dyn(t) dependent on time mainly consists of surge speed u, sway speed v, yaw angle speed r, shaft revolution n and rudder angle δ, etc.

Ship manoeuvrability is usually determined by course changing and keeping ability which is critically characterized by the turning diameter D and advance at 90 degree heading A _d obtained by:

(11)$$\displaystyle{{D({\bf \Theta} (t))} \over L} = \left( {\displaystyle{{V(t)} \over L}} \right)\displaystyle{2 \over {|K({\bf \Theta} (t))\delta _0 (t)|}},{\rm} \delta _0 (t) \ne 0$$

(12)$$\eqalign{\displaystyle{{A_d ({\bf \Theta} (t))} \over L} = &\left( {\displaystyle{{V(t)} \over L}} \right)\cr & \times\left( {T_1 ({\bf \Theta} (t)) + T_2 ({\bf \Theta} (t)) - T_3 ({\bf \Theta} (t)) + \displaystyle{{t_1 (t)} \over 2} + \displaystyle{1 \over {|K({\bf \Theta} (t))\delta _0 (t)|}}} \right),{\rm} \delta _0 (t) \ne 0}$$

where:

• δ ₀(t) denotes command rudder angle in the process of turning circle manoeuvre.

• t ₁(t) is the time for the rudder turning from amidships (zero) to the command angle δ ₀(t), and can be derived from the model of steering characteristics as follows:

  (13)$$T_E \dot \delta + \delta = \delta _0 (t),{\rm where} |\delta |,|\delta _0 | \leqslant 35^{\circ}\ {\rm and}\ |\dot \delta | \leqslant 3^{circ} /s$$

where T _E is steering time constant and usually chosen as 2·5 seconds.

Rationally, we can select the ship dynamic domain boundary as the maximum area covered by the ship with 90° course changing with time-varying speed V(t) and command rudder angle δ ₀(t). However, note that D(Θ(t)) and A _d(Θ(t)) would become infinity if |δ ₀(t)| tends to zero. It implies that the obtained D(Θ(t)) and A _d(Θ(t)) would be meaningless when |δ ₀(t)| keeps less than a threshold Δ (i.e. 5°). In order to circumvent this problem, we restrict the DQSD boundary partially dependent on |δ ₀(t)| to be the one determined by the threshold Δ whenever the command rudder angle |δ ₀(t)| is less than Δ. As a consequence, the ship submodel Q(Θ(t)) could be described as follows:

(14)$${\bi Q}({\bf \Theta} (t)) = [R_{\,fore} ({\bf \Theta} (t)),R_{aft} ({\bf \Theta} (t)),R_{starb} ({\bf \Theta} (t)),R_{\,port} ({\bf \Theta} (t))]^{\rm T} $$

where:

(15)$$\left\{ {\matrix{ {R_{\,fore} ({\bf \Theta} (t)) = L + A_d ({\bf \Theta} (t))} \hfill \cr {R_{aft} ({\bf \Theta} (t)) = L + {\textstyle{1 \over 2}}D({\bf \Theta} (t))} \hfill \cr {R_{starb} ({\bf \Theta} (t)) = B + {\textstyle{1 \over 2}}D({\bf \Theta} (t))} \hfill \cr {R_{\,port} ({\bf \Theta} (t)) = B + {\textstyle{1 \over 2}}\alpha D({\bf \Theta} (t))} \hfill \cr}} \right.$$

where:

• 0<α ⩽ 1 is the predefined coefficient which is used to sufficiently consider the influence from the International Regulations for Preventing Collisions at Sea (COLREGS) rules.

Time-varying parameters D(Θ(t)) and A _d(Θ(t)) could be determined by Equations (11) and (12), respectively.

3.2. The Human Factor Submodel

Essentially, ship domain models possess subjectivity which would be subject to human factors (i.e., navigator's influences) to some extent. In this case, human reliability analysis is the reasonable candidate to be considered to contribute to the human factor submodel of DQSD model. The popular human reliability model dependent on time can be described as follows:

(16)$$R(t) = {\rm exp}\left( { - \int\limits_0^t {E(\tau )d\tau}} \right)$$

where, E(t) denotes behaviour error rate which can be a constant or time dependent function.

Usually, E(t) is selected as a Weibull probability density function given by:

(17)$$E(t) = \displaystyle{\beta \over \eta} \left( {\displaystyle{t \over \eta}} \right)^{\beta - 1} {\rm exp}( - (t/\eta )^\beta )$$

where, β and η are shape and scale parameters of the Weibull function, respectively. Substituting Equation (17) into Equation (16), we obtain:

(18)$$R(t) = {\rm exp}({\rm exp}( - (t/\eta )^\beta ) - 1)$$

However, the above mentioned function at Equation (18) is time dependent rather than human states dependent. Note that the time variable in Equation (18) could be substituted by a virtual scale variable ρ, which is determined by the navigator's state variables. As a consequence, the navigator reliability model could be established as follows:

(19)$$R({\bf \Xi} (t)) = \exp \left( {\exp \left( { - \left( {\displaystyle{{\rho ({\bf \Xi} (t))} \over \eta}} \right)^\beta} \right) - 1} \right)$$

(20)$$\rho = {\bf \Gamma} ^{\rm T} {\bf \Xi} (t)$$

where:

• Ξ(t) = [ξ ₁(t), ξ ₂(t), …, ξ _n(t)]^T ∈Rⁿ (−1 ⩽ ξ _i(t) ⩽0) is the ship navigator state vector including skill ability, physical and mental states, etc., which would be time-varying variables.

• Γ = [γ ₁, γ ₂, …, γ _n]^T ∈Rⁿ is the weight vector with compatible dimensionality satisfying that 0 < γ _i <1.

Based on the navigator reliability model, the human factor submodel of DQSD could be implemented by:

(21)$$k({\bf \Xi} (t)) = \displaystyle{1 \over {\exp \left( {\exp \left( { - ({\bf \Gamma} ^{\rm T} {\bf \Xi} (t)/\eta )^\beta} \right) - 1} \right)}}$$

where the scale and shape parameters could be reasonably selected as η = ||Γ||₁ and β = 1, respectively.

3.3. The Circumstance Submodel

In order to consider weather conditions and navigation circumstances which would rationally contribute to the proposed DQSD model, we consider the circumstance submodel to complete the whole DQSD model. Intuitively, we describe the environment states as vector Ω(t) = [ω ₁(t), ω ₂(t), …, ω _n(t)]^T, where ω _i(t) denotes time-varying environment states including visibility, wind force, wave and traffic congestion, etc. Note that these dynamic environmental state variables are essentially qualitative and imprecise knowledge obtained from artificial assessment, which cannot be well identified by traditional methods. To the contrary, fuzzy systems are usually considered as effective tools for dealing with uncertainty information. In this case, the circumstance submodel with navigation environment assessment being output could be well modelled by using fuzzy sets theory. To be specific, all the input variables ω _i(t) are normalized into the unity interval [0, 1] and labelled by corresponding fuzzy sets A _ij(ω _i(t)) described Gaussian membership functions:

(22)$$A_{ij} (\omega _i (t)) = \exp \left( {\displaystyle{{(\omega _i (t) - c_{ij} )^2} \over {\sigma _{ij}^2}}} \right)$$

where, ω _i(t), i = 1,2,3,4, denote environment states including visibility, wind force, wave and traffic congestion, respectively.

The output variable, environment assessment, denoted by C(Ω(t)) falls into the interval [1–ζ, 1+ζ] around one, whereby 0<ζ<1. For simplicity, we consider each input variable is uniformly partitioned by only two fuzzy sets, respectively, i.e. c _ij ∈{0, 1} and σ _ij = 0·5, j = 1,2. And, the output variable is uniformly partitioned by five fuzzy sets B _k, k = 1,2,…,5, which are singletons, i.e. B _k∈{0·6, 0·8, 1, 1·2, 1·4}. Hence, fuzzy rules could be intuitively described as follows:

(23)$${\Rule\ l}\!:If\;\omega _1 (t)\;is\;A_{1j_1} (\omega _1 (t))\;and \ldots and\;\omega _4 (t)\;is\;A_{4j_4} (\omega _1 (t)),\;Then\;C({\bf \Omega} (t)){\kern 1pt} is{\kern 1pt} B_{k_l} $$

It follows that the whole fuzzy systems for modelling the circumstance submodel could be established as follows:

(24)$$C({\bf \Omega} (t)) = \displaystyle{{\sum\limits_l {B_{k_l} \varphi _l ({\bf \Omega} (t))}} \over {\sum\limits_l {\varphi _l ({\bf \Omega} (t))}}} $$

where φ _l is the aggravated activation function given by:

(25)$$\phi _l ({\bf \Omega} (t)) = \prod\limits_{i = 1}^4 {A_{i,j_i} (\omega _i (t))} $$

4. SIMULATION STUDIES

In order to demonstrate the effectiveness of the proposed DQSD model, comprehensive simulation studies will be conducted on the well-known Esso Osaka tanker in several scenarios. The principal dimensions of Esso Osaka tanker are listed in Table 1. And, ship dynamic states are mainly considered as ship speed V and command rudder angle δ ₀, where V ∈ [5kn, 25kn] and |δ ₀| ∈ [5°, 35°]. Navigator state variables are selected as skill ability ξ ₁, physical level ξ ₂ and mental level ξ ₃, where ξ _i∈[−1, 0]. The environment states are chosen as visibility ω ₁, wind force ω ₂, wave ω ₃ and traffic congestion ω ₄, where ω _i∈[0, 1]. To be specific, the chosen parameters of human, ship and environment subsystems are shown in Table 2. Without loss of generality, we simply choose parameter Γ as Γ=[0·25, 0·25, 0·25, 0·25]^T.

Table 1.

The principal dimensions of Esso Osaka tanker.

Table 2.

The principal dimensions of Esso Osaka tanker.

As the following simulation studies, the submodels of ship, human and environment will be investigated to validate the effectiveness of all the submodels which contribute to the integrated DQSD model. As a whole, typical situations will be studied to demonstrate the final performance of the DQSD model.

Firstly, simulation studies focus on the ship submodel of the DQSD model, whereby simulation results are shown in Figure 1. We can find that the scale parameters (domain radii) sharply decrease with increasing command rudder angle and decreasing ship speed. To be specific, the monotonous relationship becomes flat while the rudder angle exceeds 20° and the ship speed falls below 15 knots, especially for the fore radius R _fore. The foregoing results apparently coincide with the subjective and objective practices in marine traffic.

Figure 1.

Simulation results for ship submodel of DQSD with ship speed and rudder angle being inputs, and (a) R _fore, (b) R _aft, (c) R _starb and (d) R _port as outputs.

Secondly, we consider the human submodel of DQSD model which identifies the ship navigator's factors including skill, physical and mental levels. Note that it is impossible to show the complete input-output relationship of the human submodel with three inputs and one output in three-dimensional space. Alternatively, we turn to visually present the underlying nonlinearity of the output k partially dependent on each pair of input variables. The simulation results are shown in Figure 2, from which we can see that the shape parameter k decreases with increasing inputs, skill level, physical and mental states, monotonously. It means that the shape of the DQSD would become ‘fatter’ and consequently conservative while the states of the navigator get worse. On the contrary, the shape would be much ‘thinner’ and progressive while the navigator's states become better. In addition, it should be noted that three inputs, i.e., skill level, physical and mental states, are considered to possess equal influences on the shape of the DQSD. It obviously follows that the human submodel reveals the underlying navigator's characteristics affecting the ship domain model.

Figure 2.

Simulation results for human submodel of DQSD with skill, physical and mental levels being inputs, and shape parameter k as the output.

The circumstance submodel of the DQSD model is demonstrated to be effective via simulation studies, whereby the results are shown in Figure 3. Similar to the presentation methodology used in human submodel simulations, six pairwise visual presentations are also decomposed from the complete circumstance submodel with four input variables, i.e., visibility, wind force, wave and traffic congestion. Considering pairs of inputs for the circumstance submodel, the environment parameter C partially dependent on two out of four input variables in the whole DQSD model (6) could be visualized in a straightforward manner. From Figure 3, it can be seen that the parameter C is in inverse proportion to the environment state. To be specific, it reveals that the environment influence considered in this paper would be higher while the visibility becomes worse, and wind force, wave and traffic congestion become much more severe. As a result, the ship domain would be enlarged by increasing the parameter C which is subject to the circumstance severity.

Figure 3.

Simulation results for circumstance submodel of DQSD with visibility, wind force, wave and traffic congestion being inputs, and environment assessment C as the output.

Furthermore, we conduct simulation studies on the whole DQSD model integrated by the foregoing ship, human and circumstance submodels. Without loss of generality, in order to clearly demonstrate the resulting DQSD model, we firstly consider several typical stationary situations that human factor parameters are selected as Ξ = [0, 0, 0]^T, Ξ = [−0·2, −0·2, −0·2]^T and Ξ = [−1, −1, −1]^T, ship speeds are selected as 15, 20 and 25 knots, and circumstance parameters are selected as Ω = [1, 0, 0, 0]^T and Ω = [0, 1, 1, 1]^T, respectively. The results are shown in Figure 4, from which we could find that the ship domain scale is determined by ship factors and circumstance states, respectively, while the ship domain shape is influenced by navigator's states. To be specific, on the one hand, the scale of the DQSD model would be increased with increasing ship speed and deteriorating circumstance states. On the other hand, the shape of the DQSD model would be increased with decreasing the navigator's abilities and levels. It follows that the abovementioned investigations are evidently identical to the essential characteristics of ship domains.

Figure 4.

Simulation results for the DQSD with different stationary situations.

In order to demonstrate the dynamic performance of the entire DQSD model, we hereby consider arbitrary time-varying navigational situations whereby input signals are governed as follows: human factors Ξ(t) = [–0·5sin(0·1πt) – 0·5, 0·5sin(0·5πt) – 0·5, –0·5sin(0·4πt) – 0·5]^T, ship speed V(t) = 15 + 10sin(0·2πt), command rudder angle δ ₀(t) = 35sin(0·1πt), and circumstance influences Ω(t) = [0·5sin(0·5πt) +0·5, –0·5sin(0·4πt) +0·5, 0·5sin(0·3πt) +0·5, –0·5sin(0·2πt) +0·5]^T, respectively. Accordingly, simulation results of dynamic scale and shape parameters, i.e., Q(t) and k(t), in the DQSD model are shown in Figure 5, from which we can see that the scale quaternion Q and shape index k are dynamic simultaneously while time-varying perspective factors from human, ship and circumstance are considered. Specifically, the dynamics of the fore radius R _fore tends to be significant in the scale quaternion of the DQSD model, and thereby identical to the reality that the fore sector of the ship domain is preferably kept clear. For the shape parameter k, the dynamic characteristics illustrate the conservatism of the current DQSD model which is mainly related to the navigator states. The resulting dynamic performances of the DQSD model are shown in Figure 6, whereby ten discrete DQSD-type ship domains are depicted along the time axis. It can be seen that the DQSD model can be able to dynamically reflect time-varying situations. Actually, the continuous dynamics of the DQSD model could be considered as a set of instant stationary DQSD-type ship domains corresponding to each time point. As shown in Figure 4, the effectiveness of DQSD models with stationary situations has been clearly evaluated. In addition, both scales and shapes of the DQSD model are adaptive to changing input signals from human, ship and circumstance, respectively. It follows that the DQSD-type ship domains achieve convincing dynamic performances.

Figure 5.

The dynamic scale and shape parameters of the DQSD model.

Figure 6.

Dynamic simulation results for the DQSD model with time-varying situations.