Method for generating cargo handling transport path, cargo handling transport crane, and cargo handling transport method
US-2024109757-A1 · Apr 4, 2024 · US
US12346137B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12346137-B2 |
| Application number | US-202418886699-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 16, 2024 |
| Priority date | Mar 29, 2024 |
| Publication date | Jul 1, 2025 |
| Grant date | Jul 1, 2025 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A method for collaborative heave compensation control of a dual ship-mounted hoisting arm system including two vertical hoisting arms and two horizontal hoisting arms is provided, in which a dynamic model of the hoisting arm system is constructed based on hoisting arm position and velocity and an attitude angle of a load of the hoisting arm system; and based on the dynamic model, an optimal control strategy is obtained according to a control objective and an optimization objective under multiple constraint conditions to control the hoisting arm action, where the control objective is to track a hoisting arm reference compensation trajectory during the heave motion, the optimization objective is to minimize a tracking error, and the constraint conditions include a hoisting arm action constraint, and a position and velocity constraint of each hoisting arm after action. A system for implementing such method is also provided.
Opening claim text (preview).
What is claimed is: 1. A method for collaborative heave compensation control of a dual ship-mounted hoisting arm system, the dual ship-mounted hoisting arm system comprising a first vertical hoisting arm, a second vertical hoisting arm, a first horizontal hoisting arm and a second horizontal hoisting arm, and the method comprising: constructing a dynamic model of the dual ship-mounted hoisting arm system according to a first state variable and a second state variable; wherein the first state variable represents a position and velocity of each of the first vertical hoisting arm, the second vertical hoisting arm, the first horizontal hoisting arm and the second horizontal hoisting arm; and the second state variable is an attitude angle of a load of the dual ship-mounted hoisting arm system, and is expressed based on the position and velocity of each of the first vertical hoisting arm, the second vertical hoisting arm, the first horizontal hoisting arm and the second horizontal hoisting arm; based on the dynamic model, obtaining an optimal control strategy according to a control objective and an optimization objective under a plurality of constraint conditions; wherein the control objective is to track a reference compensation trajectory of each of the first vertical hoisting arm, the second vertical hoisting arm, the first horizontal hoisting arm and the second horizontal hoisting arm during a heave motion process; the optimization objective is to minimize a tracking error; and the plurality of constraint conditions comprise an action constraint of each of the first vertical hoisting arm, the second vertical hoisting arm, the first horizontal hoisting arm and the second horizontal hoisting arm, and a position and velocity constraint of each of the first vertical hoisting arm, the second vertical hoisting arm, the first horizontal hoisting arm and the second horizontal hoisting arm after action; and controlling an action of each of the first vertical hoisting arm, the second vertical hoisting arm, the first horizontal hoisting arm and the second horizontal hoisting arm; wherein the attitude angle α of the load is expressed as: {dot over (α)}= ġ ( a 1 ) {dot over (a)} 1 +ġ ( b 1 ) {dot over (b)} 1 +ġ ( b 2 ) {dot over (b)} 2 +ġ ( a 2 ) {dot over (a)} 2 ; and the dynamic model is simplified into: M ( q i ) q ¨ i + C ( q i , q . i ) q . i + G ( q i ) = f i i = 1 , 2 , 3 , 4 ; M ( q i ) = N T M ( q j ) N , C ( q i , q . i ) = N T C ( q j , q . j ) N ; G ( q i ) = N T G ( q j ) , f i = N T f j ; and N
Related publications grouped by family.
Answers are generated from the same data shown on this page.