Interactive Emergency Landing Guidance With Real-Time Pilot Feedback

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

In emergency situations where a pilot becomes incapacitated, individuals with limited or no flying experience face challenges in identifying and implementing appropriate aircraft control mechanisms for safe landing, leading to an increased risk of adverse incidents due to lack of feedback on proper landing instruction implementation.

Innovation Solution

An interactive emergency landing assistance system that receives a pilot incapacitation indication, transmits aircraft state data to a ground station, receives landing instructions, determines elapsed time for instruction implementation, generates implementation details, and updates instructions based on real-time aircraft state data, using a controller circuit with display devices and avionic systems to guide users through the landing process.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a crew member or passenger with minimal or no flying experience assumes responsibility for landing the aircraft, then the aircraft can be landed safely in emergency situations, but the individual faces challenges in identifying and implementing appropriate aircraft control mechanisms

Engineering Contradiction:
Improvesafe landingVSAvoididentification and implementation of control mechanisms
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The system provides real-time feedback to the user by monitoring aircraft state data and comparing it with expected states after landing instructions are executed. The system tracks whether landing instructions have been properly implemented and provides feedback on the current aircraft state, enabling users with minimal experience to understand the effects of their control actions.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system acts as an intermediary between the user and the complex aircraft control systems. It translates high-level landing instructions into specific control mechanism actions, and monitors the aircraft state to confirm proper execution, shielding the user from the complexity of directly interacting with multiple aircraft control systems.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Ease of operation

If traditional landing instructions are provided without interactive feedback, then the procedure is simple to implement, but lack of feedback regarding proper implementation leads to increased risk of adverse incidents

Engineering Contradiction:
Improvesimplicity of procedureVSAvoidsafe landing
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The system continuously monitors aircraft state data and provides feedback to the user about whether landing instructions have been properly implemented. This feedback loop allows the system to detect when instructions have not been executed correctly and prompt the user to make necessary corrections, thereby improving safety without significantly complicating the procedure.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system automatically monitors and tracks the execution of landing instructions by itself, without requiring additional manual verification steps from the user. The system self-updates on aircraft state changes and determines whether instructions have been implemented, reducing the cognitive burden on the user while maintaining safety through automated monitoring.

Inventive Principle:
Principle #25Self-service

3Reliability

If an interactive system with real-time monitoring and feedback is implemented, then the risk of adverse incidents is reduced, but the system complexity increases

Engineering Contradiction:
Improvesafe landingVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system leverages existing multi-functional avionics systems and data sources already present in modern aircraft. By utilizing existing sensors, communication systems, and flight data networks, the solution avoids adding dedicated complex hardware while achieving comprehensive monitoring and feedback capabilities through software-based integration.

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

Solution Approach 2:

The system serves as an intermediary layer that integrates with existing aircraft systems without requiring fundamental changes to their architecture. It accesses data from multiple existing systems through standardized interfaces and provides unified feedback, thereby reducing overall system complexity by consolidating multiple functions into a single coordinating layer.

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS20250232683A1Systems and methods for providing interactive emergency landing assistance
Publication Date: 2025.07.17 HONEYWELL INTERNATIONAL INC
  • US20250232683A1 patent drawing
  • US20250232683A1 patent drawing
  • US20250232683A1 patent drawing

AI summary

Systems and methods are provided for providing interactive emergency landing assistance. Receiving a pilot incapacitation indication. Receiving aircraft state data from at least one avionics system of an aircraft. Transmitting an emergency landing assistance request and the aircraft state data to the ground station. Receiving a first landing instruction based on the aircraft state data from the ground station. Determining whether a pre-defined period of time has elapsed without implementation of the first landing instruction. Generating instruction details associated with the implementation of the first landing instruction based on the determination. Receiving updated aircraft state data from the at least one avionics system following the implementation of the first landing instruction. Transmitting the updated aircraft state data to the ground station. Receiving a second landing instruction based on the updated aircraft state data from the ground station.