Predictive Altitude Alerting for Aircraft Descent Trajectories

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Solution Overview

Problem

Current ground proximity warning systems (GPWS) lack sufficient lead time in alerting pilots of descent below altitude events and provide limited enhanced situation awareness for flight crews, particularly in predicting premature descents below minimum sector altitude, minimum safe altitude, and terrain clearance floor.

Innovation Solution

A method and system that utilize a Flight Management System (FMS) and Enhanced Ground Proximity Warning System (EGPWS) to predict aircraft movement trajectories, evaluate them against minimum altitudes, and output alerts via visual and aural indicators, providing greater lead time and enhanced awareness by modeling vertical descent paths and determining required vertical acceleration to avoid altitude convergence.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of time

If traditional GPWS is used to alert pilots of descent below altitude events, then the system provides basic ground proximity warning functionality, but the lead time for alerting pilots is insufficient

Engineering Contradiction:
Improvelead time for alerting pilotsVSAvoidalerting reliability
Core Design Contradiction:
Loss of timeVSReliability

Solution Approach 1:

The system performs preliminary evaluation of the aircraft predicted movement trajectory against minimum altitudes before the actual descent occurs. By predicting the trajectory using FMS data and evaluating it proactively against minimum sector altitude, minimum safe altitude, and terrain clearance floor, the system generates alerts in advance, providing pilots with sufficient lead time to take corrective action while maintaining high reliability through predictive analysis.

Inventive Principle:
Principle #10Preliminary action

2Loss of information

If EGPWS with TCF function is used to alert descent below terrain clearance floor, then the system provides terrain awareness, but the situation awareness for flight crew is limited

Engineering Contradiction:
Improvesituation awareness informationVSAvoidsystem complexity
Core Design Contradiction:
Loss of informationVSDevice complexity

Solution Approach 1:

The system provides enhanced feedback to the flight crew by continuously evaluating the predicted movement trajectory against multiple altitude parameters (minimum sector altitude, minimum safe altitude, terrain clearance floor) and providing comprehensive situational awareness information. This feedback mechanism delivers detailed information about potential altitude breaches and required vertical acceleration, enabling better decision-making without significantly increasing system complexity.

Inventive Principle:
Principle #23Feedback

3Loss of time

If predictive capabilities are integrated into GPWS to evaluate aircraft trajectory, then the lead time and situation awareness are improved, but the system complexity increases

Engineering Contradiction:
Improvereaction time for pilotsVSAvoidsystem integration complexity
Core Design Contradiction:
Loss of timeVSDevice complexity

Solution Approach 1:

The system achieves multi-functionality by integrating FMS (Flight Management System) and EGPWS (Enhanced Ground Proximity Warning System) capabilities into a unified alerting system. The FMS provides flight plan and trajectory prediction data, while the EGPWS evaluates this data against multiple altitude parameters (minimum sector altitude, minimum safe altitude, terrain clearance floor). This universal integration improves reaction time and situation awareness without proportionally increasing complexity, as it leverages existing system functionalities.

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

Data Source

PatentUS11830373B2Systems and methods for alerting descent below altitude
Publication Date: 2023.11.28 HONEYWELL INTERNATIONAL INC
  • US11830373B2 patent drawing
  • US11830373B2 patent drawing
  • US11830373B2 patent drawing

AI summary

Methods and system for alerting descent with respect to at least one of minimum sector altitude, minimum safe altitude and terrain clearance floor in an aircraft. The methods and systems receive at least one of a minimum sector altitude value, a minimum safe altitude value and a terrain clearance floor value based on a flight plan of the aircraft or a location of the aircraft. A movement trajectory of the aircraft is predicted. The aircraft predicted movement trajectory is evaluated with respect to the at least one of the minimum sector altitude value, the minimum safe altitude value and the terrain clearance floor value. An alert is output when the evaluation predicts convergence of the aircraft predicted movement trajectory and the at least one of the minimum sector altitude value, the minimum safe altitude value and the terrain clearance floor value.