Boom Attitude Detection Using GPS Correction Tables

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Solution Overview

Problem

Conventional boom attitude detection methods for cranes using GPS are unreliable when GPS signals are interrupted, leading to inaccurate calculations and potential safety issues during crane operations.

Innovation Solution

A boom attitude detection apparatus that employs a GPS device with base and mobile station antennas, an attitude detector, and a load detector, utilizing a correction table to calculate and correct boom attitudes even in low GPS signal conditions, ensuring continuous and accurate attitude determination.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If GPS device is used to calculate boom attitude, then positioning accuracy is improved, but reliability deteriorates when GPS signals are interrupted

Engineering Contradiction:
Improvepositioning accuracyVSAvoidreliability when GPS signals are interrupted
Core Design Contradiction:
Measurement precisionVSReliability

Solution Approach 1:

The patent introduces a correction table as an intermediary data structure that stores pre-calculated correction values. When GPS signals are available, the system calculates accurate boom attitudes and stores correction values in the table. When GPS signals are interrupted, the system retrieves correction values from the table to maintain reliable boom attitude calculation, thus resolving the contradiction between GPS positioning accuracy and reliability during signal interruption.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The system performs preliminary calculations of correction values and stores them in the correction table during periods when GPS signals are available. This preliminary action ensures that when GPS signals are later interrupted, the pre-stored correction values can be immediately applied to maintain accurate and reliable boom attitude detection without interruption.

Inventive Principle:
Principle #10Preliminary action

2Measurement precision

If correction values are updated frequently, then measurement precision is improved, but device complexity increases

Engineering Contradiction:
Improvecorrection value accuracyVSAvoidsystem complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The correction table is designed to be dynamically updated based on GPS positioning reliability. When GPS signals are reliable, the system updates the correction table with newly calculated values. When GPS signals are unreliable, the system uses existing correction values without updating. This dynamic approach maintains measurement precision while avoiding unnecessary complexity from constant updates.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentEP3214033B1Boom attitude detection device
Publication Date: 2021.10.20 TADANO LTD
  • EP3214033B1 patent drawingFigure 1
  • EP3214033B1 patent drawingFigure 2
  • EP3214033B1 patent drawingFigure 3

AI summary

Provided is a boom attitude detection device capable of determining the attitude of a boom even if a GPS device is in poor radio reception conditions. The boom attitude detection device is equipped with: a GPS device (20) that measures the position of the leading end of the boom (13); attitude detectors (31) and (32) that detect the attitude of the boom (13); and a calculation device (40). If the positioning reliability of the GPS device (20) is high, the calculation device (40) determines a correction value for correcting detection values of the attitude detectors (31) and (32) to the attitude of the boom (13) determined from the positioning value of the GPS device (20). If the positioning reliability of the GPS device (20) is low, the calculation device (40) corrects the detection values of the attitude detectors (31) and (32) using correction values and determines the attitude of the boom (13). Even if the GPS device (20) is in poor radio reception conditions and the positioning reliability is low, the attitude of the boom (13) can be determined.