FMS-TCAS Coupling for Automatic Evasive Maneuver Control

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Solution Overview

Problem

Current aircraft flight control systems face challenges in responding timely and accurately to Traffic Alert and Collision Avoidance System (TCAS) alerts, especially in congested airspace, due to high cognitive demand on pilots and limitations of automated responses, which can lead to increased frequency of evasive maneuvers and workload.

Innovation Solution

A flight management system that integrates TCAS data with navigation and autopilot systems to identify conflicts and automatically modify flight plans, speed, or flight paths to avoid collisions, and implement evasive maneuvers without pilot intervention, while ensuring safety by assessing limiting conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of time

If automated responses based on autopilot systems are used, then response time to TCAS alerts is reduced, but system cost increases and pilot oversight is required

Engineering Contradiction:
Improveresponse timeVSAvoidsystem cost
Core Design Contradiction:
Loss of timeVSDevice complexity

Solution Approach 1:

The system performs self-service by automatically generating and executing evasive maneuvers without requiring pilot intervention. The flight management system autonomously processes TCAS alerts, determines appropriate responses, and implements maneuvers, thereby reducing response time while eliminating the need for costly autopilot retrofits and pilot oversight

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The flight management system is enhanced to perform multiple functions: it processes navigation data, manages flight plans, and now also handles TCAS alert responses. This multi-functionality allows the existing FMS to provide automated collision avoidance responses without requiring separate dedicated autopilot systems, reducing overall system complexity and cost

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

2Device complexity

If pilots manually respond to TCAS alerts, then system complexity remains low, but cognitive workload increases and response time is delayed

Engineering Contradiction:
Improvesystem complexityVSAvoidpilot workload
Core Design Contradiction:
Device complexityVSEase of operation

Solution Approach 1:

The system takes over the response task from the pilot, performing self-service by automatically analyzing TCAS alerts and executing evasive maneuvers. This transfers the cognitive burden from the pilot to the flight management system, significantly reducing pilot workload while maintaining relatively simple system architecture

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system performs preliminary processing of TCAS alerts by automatically analyzing the situation and determining the appropriate evasive maneuver before pilot action is required. This preliminary automated response preparation reduces the cognitive demand on pilots and accelerates overall response time

Inventive Principle:
Principle #10Preliminary action

3Measurement precision

If navigation accuracy is improved, then flight path precision increases, but frequency of TCAS alerts increases due to closer neighbor aircraft detection

Engineering Contradiction:
Improvenavigation accuracyVSAvoidTCAS alert frequency
Core Design Contradiction:
Measurement precisionVSObject-generated harmful factors

Solution Approach 1:

The system performs preliminary conflict detection by analyzing the integrated trajectory against predicted neighbor aircraft paths before a TCAS alert is generated. This early detection allows the system to proactively modify flight plans or initiate evasive maneuvers before alerts occur, effectively reducing the frequency of actual TCAS alerts requiring pilot response

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system uses feedback from the integrated navigation and TCAS data to continuously monitor and adjust the flight path. By processing navigation accuracy data in conjunction with TCAS information, the system can make real-time adjustments to avoid conflicts, thereby reducing the frequency of alerts while maintaining precise navigation

Inventive Principle:
Principle #23Feedback

4Loss of time

If evasive maneuvers are automatically implemented, then pilot response time is reduced, but safety risks increase without pilot oversight

Engineering Contradiction:
Improveresponse timeVSAvoidsafety
Core Design Contradiction:
Loss of timeVSReliability

Solution Approach 1:

The system performs preliminary safety verification by evaluating limiting conditions and assessing the safety of proposed evasive maneuvers before automatic implementation. This preliminary safety check ensures that automatically implemented maneuvers are safe and appropriate, maintaining reliability while enabling fast automated response

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system incorporates feedback mechanisms that continuously monitor the execution of evasive maneuvers and compare actual outcomes against predicted results. This feedback loop ensures safety by detecting deviations and allowing for corrective action, enabling automatic implementation while maintaining pilot confidence and safety standards

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS11138892B2TCAS coupled FMS
Publication Date: 2021.10.05 HONEYWELL INTERNATIONAL INC
  • US11138892B2 patent drawing
  • US11138892B2 patent drawing

AI summary

An enhanced flight control system and method providing a technological improvement over a conventional flight control systems. A control module employs rules to determine whether or not a received traffic collision avoidance system (TCAS) evasive maneuver is automatically implemented. Specifically, the control module effectively couples the TCAS to the FMS, allowing access to the flight plan and to the navigation database and the approach procedures and runway data therein. An algorithm determines when there is a co-occurrence of the conditions (1) a flight plan uploaded in the FMS, (2) autopilot is engaged, (3) VNAV is engaged. Upon co-occurrence of (1) and (2) and (3), and an evasive maneuver is received from a TCAS, the control module determines whether or not to automatically implement the evasive maneuver. Look ahead algorithms may also analyse and modify the flight plan to preclude TCAS alerts and evasive procedures being required.