Electric Aircraft Simulation Boundaries With Distance-Based Flight Guidance

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Solution Overview

Problem

Pilots face challenges in determining their proximity to boundaries during flight, which can lead to unsafe and unpredictable flight experiences due to the lack of accurate distance measurement from the boundary in electric aircraft simulations.

Innovation Solution

A system comprising a sensor, a computing device, and a remote device that detects aircraft location and boundary data, calculates the distance, and provides real-time recommendations for adjustments to maintain safe flight paths, displayed to the pilot.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If no boundary detection system is used, then the flight simulation system remains simple, but the pilot cannot accurately determine distance from boundaries leading to unsafe flight operations

Engineering Contradiction:
Improveflight safetyVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system divides the boundary detection functionality into separate modular components: sensors for detecting boundary markers, a computing device for processing location data and calculating distances, and a remote device for displaying information to the pilot. This segmentation allows the system to provide comprehensive boundary awareness while maintaining manageable complexity through modular architecture.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The computing device acts as an intermediary between the sensors and the pilot. It receives raw boundary and location data from sensors, processes this information to calculate distance datums, generates recommended adjustments, and transmits this processed information to the remote device for pilot display. This intermediary layer simplifies the information flow and protects the pilot from dealing with raw complex data.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Measurement precision

If real-time boundary distance calculation is implemented, then the pilot receives accurate distance information, but the processing requirements and computational load increase

Engineering Contradiction:
Improvedistance measurement accuracyVSAvoidcomputational power
Core Design Contradiction:
Measurement precisionVSPower

Solution Approach 1:

The system pre-establishes boundary datums by detecting boundary markers before flight operations begin. The computing device stores these boundary definitions and uses them as reference points during flight. This preliminary action allows real-time distance calculations to be performed by simply comparing current location data against pre-stored boundary coordinates, significantly reducing computational load during actual flight operations while maintaining high measurement precision.

Inventive Principle:
Principle #10Preliminary action

3Loss of information

If continuous monitoring of aircraft location relative to boundaries is performed, then the pilot maintains situational awareness, but the energy consumption and data transmission increase

Engineering Contradiction:
Improveinformation accuracyVSAvoidenergy consumption
Core Design Contradiction:
Loss of informationVSUse of energy by moving object

Solution Approach 1:

The system performs boundary distance calculations and transmits recommendations to the pilot at periodic intervals rather than continuously. The computing device calculates distance datums based on aircraft location data and transmits recommended adjustments at defined time periods or when distance thresholds are crossed. This periodic operation maintains accurate boundary awareness information while significantly reducing energy consumption and data transmission requirements compared to continuous monitoring.

Inventive Principle:
Principle #19Periodic action

Data Source

PatentUS11789441B2System and method for defining boundaries of a simulation of an electric aircraft
Publication Date: 2023.10.17 BETA AIR LLC
  • US11789441B2 patent drawing
  • US11789441B2 patent drawing
  • US11789441B2 patent drawing

AI summary

The system and method for defining boundaries of a simulation of an electric aircraft is illustrated. The system comprises a sensor, a computing device, and a remote device. The sensor is configured to detect an aircraft location datum, detect a boundary datum associated with a three-dimensional flying space, and transmit the aircraft location datum and boundary datum to a computing device. The computing device is configured to receive the aircraft location datum and boundary datum from the sensor, determine a distance datum between the aircraft location and boundary as a function of the aircraft location datum and boundary datum generate a recommended aircraft adjustment as a function of the distance datum, and transmit the distance datum and recommended aircraft adjustment to a remote device. The remote device is configured to receive the distance datum and recommended aircraft adjustment and display them to a user.