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Development of a Decision Support System in Ship-To-Ship Lightering

Published online by Cambridge University Press:  28 March 2016

Dagfinn Husjord*
Affiliation:
(UiT The Arctic University of Norway)
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Abstract

This paper focusses on the development of a tool for decision-making, tailored for personnel involved in complex Ship-To-Ship (STS) operations, to enhance the efficiency and safety of these operations. A step-wise approach has been selected. The first step includes specification, development and testing of the tool in a simulated work environment using full-mission simulators. In the second step the findings from application of the tool in the simulated work environment will be used to develop a prototype which will be tested during real life STS operations. This paper describes work done in the first of these two steps. During four iterations, a Graphical User Interface (GUI) has been made following Interaction Design (IxD) principles. The designs have been iteratively developed and tested by experienced ship's officers in a ship-handling simulator to clarify key information to enhance their Situation Awareness (SA) and decision-making process. In order to find indicators for performance, an initial performance test was carried out in a ship-handling simulator. The test indicates that a logic based Decision-Support System (DSS) can improve existing simulator-based training activities in STS operations.

Information

Type
Review Article
Copyright
Copyright © The Royal Institute of Navigation 2016 
Figure 0

Figure 1. The principles of a standard approach manoeuvre in STS lightering operations (left) (OCIMF and ICS, 2005). Images of the landing phase (Courtesy of SPT Ltd).

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Figure 2. Radar images from the final phase (Pedersen et al., 2010).

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Figure 3. Steps in the natural intuitive decision-making process in navigation.

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Figure 4. Mapping the span of approaches to IxD (Sanders and Stappers, 2008).

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Figure 5. Spatial experience enables the mooring master to “see the vessels’ movements before his inner eye”. (Courtesy of SPT Ltd).

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Figure 6. A model of the decision-making cycle in STS lightering with experience, situational and spatial awareness as the underlying layers.

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Figure 7. Improvement of SA in the decision-making cycle.

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Figure 8. The iterative IxD-cycle used in the development of the GUI.

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Figure 9. Paper prototypes of the second iteration.

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Figure 10. A sketch used for discussions with the mooring masters.

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Figure 11. GUI alternative 1. Paper prototypes (left) and a screen shot of the tablet PC (right).

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Figure 12. GUI alternative 2. Paper prototypes (left) and a screen shot of the tablet PC (right).

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Table 1. Example of questionnaire for one parameter.

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Table 2. The seven parameters with sub questions are scaled from 1 to 9 by the users A, B and C, in the third iteration, and by the users D, E, F and G in the fourth iteration.

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Figure 13. Screen shots of the fourth and final iteration. (a) The vessels in the approach phase. (b) Closer to the landing. (c) In the landing phase the longitudinal distance to the hose connection-point can be seen in the indicator to the right. The SS has to move 7·5 (m) ahead to come into position to moor. (d) The SS has landed in position, just 1·9 (m) in front of the STBL's hose connection-point.

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Figure 14. System structure. (Courtesy of UiT The Arctic University of Norway).

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Figure 15. The criteria and optimum track to follow in the test scenario, presented in sketches from Position 1 to Position 5.

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Figure 16. (a) Deviations from one cable off. (b) Transverse stern speed, $\; {\left\vert {\dot \eta} \right\vert_{Aft}}$, in the landing.

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Figure 17. Rudder commands, δ, and transverse stern speed, $\; {\left\vert {\dot \eta} \right\vert_{Aft}}$, during the landing, DSS test group.

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Figure 18. Rudder commands, δ, and transverse stern speed, $\; {\left\vert {\dot \eta} \right\vert_{Aft}}$, during the landing. STD test group.

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Figure 19. Variance, σ2, of the transverse stern speed, $\; {\left\vert {\dot \eta} \right\vert_{Aft}}$, during the landing phase.

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Figure 20. A recorded plot from the nine last minutes of a DSS users’ landing.

Supplementary material: File

Husjord supplementary material

Appendix

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