UAS Design Control Circuit for Component Compatibility

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Solution Overview

Problem

The existing technologies for designing and assembling unmanned aircraft systems (UAS) lack efficiency in customizing UAS components based on specific tasks, often requiring extensive knowledge and time, leading to potential defects due to incorrect component selection and assembly.

Innovation Solution

A system comprising a UAS component database and a design control circuit that identifies primary and secondary components based on task parameters, providing a design plan for assembling UAS components that cooperate to perform intended tasks, with options for customization and simulation for certification.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If traditional manual design and assembly methods are used for UAS, then users have flexibility in component selection, but the process requires extensive knowledge and time, leading to potential defects due to incorrect component selection and assembly

Engineering Contradiction:
Improvecomponent selection accuracyVSAvoiddesign and assembly time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The system pre-stores compatibility information and assembly instructions for all UAS components in a database before the design process begins. When a user selects a component, the system has already prepared all necessary compatibility data, assembly instructions, and validation rules, eliminating the need for users to perform complex compatibility checks manually during the design process.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system acts as an intermediary between the user and the complex world of UAS component compatibility. It provides a user interface that translates user requirements into validated component selections, automatically checking compatibility against the database and guiding users through the assembly process with step-by-step instructions, thereby reducing both time and errors.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Adaptability or versatility

If traditional manual design and assembly methods are used for UAS, then users can customize their systems, but extensive knowledge is required leading to potential defects

Engineering Contradiction:
Improvecustomization capabilityVSAvoidassembly process complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The system segments the complex UAS design process into distinct, manageable steps: component selection, compatibility validation, assembly instruction generation, and verification. Each step is handled independently with specific guidance, breaking down the overwhelming complexity into simple, sequential tasks that users can follow without requiring expert knowledge.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system changes the parameters of interaction by providing dynamic, context-aware guidance that adapts to the specific components selected. Instead of requiring users to know all possible compatibility parameters, the system automatically adjusts the information presented based on the current selection state, showing only relevant compatibility checks and assembly steps for the specific components chosen.

Inventive Principle:
Principle #35Parameter changes

3Productivity

If automated component identification is implemented, then assembly efficiency is improved, but the system complexity increases

Engineering Contradiction:
Improveassembly efficiencyVSAvoidsystem structure
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The system employs universal data structures and communication protocols that work across all UAS component types. The database schema, compatibility validation logic, and assembly instruction generation mechanisms are designed to handle diverse components through common interfaces, reducing the need for component-specific complex handling logic and making the automated system more efficient.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Data Source

PatentUS10467376B2Unmanned aircraft systems and methods of assembly
Publication Date: 2019.11.05 WALMART APOLLO LLC
  • US10467376B2 patent drawing
  • US10467376B2 patent drawing
  • US10467376B2 patent drawing

AI summary

Some embodiments provide a system to design an unmanned aircraft system (UAS) based on an intended task, comprising: UAS component database and a design control circuit configured to: obtain a first set of multiple task parameters corresponding to a requested task that the UAS is being designed to perform; identify at least one primary type of UAS component to be included in the UAS being designed; identify a first set of one or more secondary types of UAS components to support the primary type of UAS component while implementing the task; and provide a design plan of the designed UAS designed to be utilized to implement the task.