Aircraft Software Verification Data Structure
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Solution Overview
Problem
Current systems for loading software aircraft parts onto aircraft require tedious manual checks to ensure accuracy, which is cumbersome and prone to errors.
Innovation Solution
A computer-implemented method and apparatus that uses a data structure with aircraft identification objects to verify the compatibility of software aircraft parts with specific aircraft, allowing for automated verification through a data processing system.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If manual checking of documents is used to verify software aircraft part compatibility, then verification can be performed, but the process is cumbersome and error-prone
Solution Approach 1:
The patent replaces the manual mechanical checking process with an automated computer-based system. The data structure with aircraft identification objects enables automated verification by comparing software part requirements against aircraft characteristics stored in the system, eliminating manual document checking and reducing human error.
Solution Approach 2:
The patent creates a digital copy of aircraft characteristics and software part requirements in the form of aircraft identification objects within a structured data format. This digital representation allows for automated comparison and verification without needing to handle physical documents, streamlining the verification process.
2Manufacturing precision
If detailed manual verification is performed to ensure correct software aircraft part loading, then accuracy is improved, but time consumption increases
Solution Approach 1:
The patent performs preliminary organization of aircraft characteristics and software part requirements into structured aircraft identification objects before the actual verification needs to occur. This pre-structuring of data enables rapid automated verification when needed, eliminating the need for time-consuming manual checks at the moment of software loading.
Solution Approach 2:
The patent substitutes manual verification processes with automated computer-based verification using the structured data structure. The system automatically compares aircraft identification objects with software part requirements, providing accurate verification results instantaneously without manual intervention.
3Reliability
If comprehensive aircraft specifications are tracked to ensure software compatibility, then verification capability is enhanced, but system complexity increases
Solution Approach 1:
The patent segments comprehensive aircraft specifications into discrete aircraft identification objects, each representing a specific characteristic or parameter. This segmentation allows the system to handle complex verification requirements by breaking them down into manageable, independently verifiable components within a structured data format.
Solution Approach 2:
The patent transforms comprehensive aircraft specifications into standardized parameters within aircraft identification objects. By converting diverse aircraft characteristics into a unified parameter structure, the system maintains verification capability while reducing apparent complexity through standardization.
Data Source
AI summary
A computer implemented method, apparatus, and computer usable program code for creating a data structure residing on a computer recordable medium for verifying whether a software aircraft part can be loaded. The data structure comprises a set of aircraft identification objects. An aircraft identification object within the set of aircraft identification objects contains a level of specificity about a set of aircraft on which the software aircraft part can be loaded. The set of aircraft identification objects are capable of being read from the computer recordable medium to verify whether the software aircraft part can be loaded in an aircraft.