Aircraft Trajectory Generation Centralizing Avionics Inputs

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Solution Overview

Problem

The complexity of current aircraft flight conduct systems, involving multiple independent avionics systems, increases crew workload and can lead to safety issues due to confusion and incorrect identification of system statuses, contributing to potential accidents.

Innovation Solution

A method and device that generate a resulting setpoint trajectory for aircraft, centralizing the generation of trajectory segments across multiple axes, allowing selection of operating modes to integrate and prioritize different avionics system inputs, thereby simplifying the flight management and reducing system complexity.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Extent of automation

If multiple independent avionics systems are used for flight conduct, then the functionality and automation level are improved, but the system complexity and crew workload increase

Engineering Contradiction:
Improveautomation levelVSAvoidsystem complexity
Core Design Contradiction:
Extent of automationVSDevice complexity

Solution Approach 1:

The patent merges multiple independent avionics systems (FMS, AFCS, AT, FCS) into a unified architecture where a central trajectory generation device integrates trajectory segments from different sources. This consolidation maintains the functional capabilities of each system while reducing overall system complexity and improving coordination between subsystems.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The trajectory generation device serves as a universal platform that handles multiple functions: it generates trajectory segments, selects optimal segments based on operating modes, and coordinates with various avionics systems. This multi-functional approach replaces the need for separate specialized systems, reducing complexity while maintaining automation capabilities.

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

2Extent of automation

If multiple independent avionics systems are used for flight conduct, then the automation capabilities are enhanced, but the crew workload increases

Engineering Contradiction:
Improveautomation capabilitiesVSAvoidcrew workload
Core Design Contradiction:
Extent of automationVSEase of operation

Solution Approach 1:

The central trajectory generation device acts as an intermediary between the crew and multiple avionics systems. It manages the complexity of coordinating FMS, AFCS, AT, and FCS, presenting a simplified interface to the crew while maintaining enhanced automation capabilities through systematic integration.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Adaptability or versatility

If multiple independent avionics systems are used, then the functional capabilities are improved, but confusion and safety risks increase

Engineering Contradiction:
Improvefunctional capabilitiesVSAvoidflight safety
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The patent segments the trajectory into multiple trajectory segments, each generated by different avionics systems according to specific operating modes. This segmentation allows each system to contribute its specialized functionality while the central coordination ensures safe and coherent integration, reducing confusion and improving overall flight safety.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS10055999B2Method and device for generating a resulting setpoint trajectory of an aircraft, related computer program product and aircraft
Publication Date: 2018.08.21 THALES SA
  • US10055999B2 patent drawing
  • US10055999B2 patent drawing
  • US10055999B2 patent drawing

AI summary

This method makes it possible to generate a resulting setpoint trajectory of an aircraft, a guiding system controlling the trajectory of the aircraft relative to the resulting setpoint trajectory.The generating method is implemented by an electronic device and comprises selecting at least one mode from among several operating modes, acquiring a setpoint trajectory prepared by a flight management system, obtaining an alternative setpoint trajectory from an element from among a module for computing a trajectory and an external generating system, and generating the resulting setpoint trajectory, which includes one or several segments of the alternative setpoint trajectory for the period of time corresponding to the selection of another mode.