Dynamic positioning systems and methods

Patent metadata

Field	Value
Publication number	US-9195234-B2
Application number	US-201314085852-A
Country	US
Kind code	B2
Filing date	Nov 21, 2013
Priority date	Nov 21, 2013
Publication date	Nov 24, 2015
Grant date	Nov 24, 2015

Abstract

Dynamic positioning systems and methods for controlling thrusters of a vessel. A dynamic positioning system includes a controller configured to predict position and heading of the vessel and efficiently control the the thrusters based on the predicted position and heading.

First claim

What is claimed is:

1. A dynamic positioning system, comprising
a controller configured to control thrusters, comprising:
a processor; and
a memory having stored thereon computer-executable instructions which, when executed by the processor, cause the processor to perform operations comprising:
predicting, by the processor, a maximum radial position error and a final radial position error, wherein the maximum radial position error is a maximum distance between a position of a vessel and a target position during a time period, and wherein the final radial position error is a distance between the position of the vessel and the target position at an end of the time period; and
calculating, by the processor, thrust forces for efficient control when each of:
a start position is inside a working area, wherein the start position is the position of the vessel at a beginning of the time period;
the maximum radial position error is inside a operating area;
the final radial position error is inside the working area;

the calculating the thrust forces for efficient control comprising calculating, by the processor, thrust forces that are substantially constant with respect to thrust forces at a previous time step;
calculating, by the processor, thrust forces for scaled control when the start position is outside the working area the calculation including a gain that is scaled based on a distance between the start position and an edge of the working area and wherein
the gain is scaled by a multiplier based on:
γ=( p start −R in )/( R out −R in )

wherein pstart is the start position, Rin is a radius of the working area, and Rout is a radius of the operating area.

2. The dynamic positioning system of claim 1 , wherein the gain is a proportional gain.

3. The dynamic positioning system of claim 1 , wherein the gain is a velocity gain.

4. The dynamic positioning system of claim 1 , the memory having stored thereon computer-executable instructions which, when executed by the processor, cause the processor to perform operations comprising:
calculating, by the processor, thrust forces for optimized control when:
the start position is inside the working area and at least one of:
the maximum radial position error is outside the operating area; and
the final radial position error is outside the working area;

the calculation including minimizing a cost function, wherein the cost function is based on a distance between the final radial position error and an edge of the working area.

5. The dynamic positioning system of claim 4 , wherein the cost function is further based on a difference between thrust force and an opposed external force.

6. The dynamic positioning system of claim 5 , wherein a weight is applied to the distance between the final radial position error and the edge of the working area, wherein the weight is larger than one.

7. The dynamic positioning system of claim 4 , wherein the cost function is based on:
J =( F tx +F ex ) 2 +( F ty +F ey ) 2 +W ( p end −R in )
where F tx is a sway thrust force, F ty is a surge thrust force, F ex is a sway external force, F ey is a surge external force, p end is the final radial position error, Rin is a radius of the working area, and W is a weight.

8. The dynamic positioning system of claim 1 , the memory having stored thereon computer-executable instructions which, when executed by the processor, cause the processor to perform operations comprising:
predicting, by the processor, a maximum heading error and a final heading error, wherein the maximum heading error is a maximum angle between a heading of a vessel and a nominal aim during a time period, and wherein the final heading error is an angle between the heading of the vessel and the nominal aim at an end of the time period; and
calculating, by the processor, a thrust moment for efficient control when each of:
a start heading is inside a working angle range, wherein the start heading is a heading of the vessel at a beginning of the time period;
the maximum heading error is inside an outer limit of an operating angle range; and
the final heading error is inside an inner limit of the working angle range;

the calculating the thrust moment for efficient control comprising calculating, by the processor, a thrust moment that is substantially constant with respect to a thrust moment at a previous time step.

9. The dynamic positioning system of claim 8 , the memory having stored thereon computer-executable instructions which, when executed by the processor, cause the processor to perform operations comprising:
calculating, by the processor, a thrust moment for scaled control when the start heading is outside the working angle range; the calculation including a gain that is scaled based on a distance between the start heading and an inner limit of the working angle range.

10. The dynamic positioning system of claim 9 , wherein the gain is a proportional gain.

11. The dynamic positioning system of claim 9 , wherein the gain is a velocity gain.

12. The dynamic positioning system of claim 9 , wherein the gain is scaled by a multiplier based on:
γ=(ψ start −δ in )/(δ out −δ in )

wherein ψstart is the start heading, in is an inner limit of the working angle range, and δout is an outer limit of an operating angle range.

13. The dynamic positioning system of claim 9 , the memory having stored thereon computer-executable instructions which, when executed by the processor, cause the processor to perform operations comprising:
calculating, by the processor, a thrust moment for optimized control when:
the start heading is inside the working angle range and at least one of:
the maximum heading error is outside the outer limit of the operating angle range; and
the final heading error is outside the inner limit of the working angle range;

the calculation including minimizing a cost function, wherein the cost function is based on a distance between the final heading error and the inner limit of the working angle range.

14. The dynamic positioning system of claim 13 , wherein the cost function is further based on a difference between the thrust moment and an opposed external moment.

15. The dynamic positioning system of claim 14 , wherein a weight is applied to the distance between the final heading error and the inner limit of the working angle range, wherein the weight is larger than one.

16. The dynamic positioning system of claim 13 , wherein the cost function is based on:
J =( F th +F eh ) 2 +W (ψ end −δ in )

where F th is the thrust moment, F eh is an external moment, ψ end is a final heading, δin is the inner limit, and W is a weight.

17. A dynamic positioning system, comprising
a controller configured to control thrusters, comprising:
a processor; and
a memory having stored thereon computer-executable instructions which, when executed by the processor, cause the processor to perform operations comprising:
predicting, by the processor, a maximum heading error and a final heading error, wherein the maximum heading error is a maximum angle between a heading of a vessel and a nominal aim during a time period, and wherein the final heading error is an angle between the heading of the vessel and the nominal aim at an end of the time period; and
calculating, by the processor, a thrust moment for efficient control when each of:
a start heading is inside a working angle range, wherein the start heading is a heading of the vessel at a beginning of the time period;
the ma

Assignees

• Ge Energy Power Conversion Technology Ltd
• Ge Energy Power Conversion Technology Ltd

Inventors

• Stephens Richard Ian

Classifications

• G05D1/0208 Primary

  dynamic anchoring · CPC title

• B63H25/42

  Steering or dynamic anchoring by propulsive elements (by jets B63H25/46); Steering or dynamic anchoring by propellers used therefor only; Steering or dynamic anchoring by rudders carrying propellers · CPC title