Aircraft Vertical Path Generation for Energy-Constrained Descent

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Solution Overview

Problem

Current aircraft energy management during descent and approach phases is labor-intensive for pilots, leading to potential overshooting or undershooting of target points, especially in dynamic environments with obstacles, resulting in increased workload and time wastage due to go-arounds.

Innovation Solution

A method and device that automatically generate an optimized vertical flight path by iteratively processing possible flight strategies, validating path segments for obstacle avoidance, and scoring based on cost and proximity to a target state, ensuring collision-free and energy-constrained paths between the current and target states.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If pilots manually manage aircraft energy during descent and approach, then they can adapt to varying flight conditions, but the workload increases and the risk of human error rises

Engineering Contradiction:
Improvepilot workloadVSAvoidenergy management accuracy
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The system enables self-service by automatically generating and optimizing vertical flight paths without requiring pilot intervention. The flight management system autonomously computes optimal descent profiles, manages energy constraints, and adjusts flight parameters, allowing the aircraft to 'serve itself' during the critical approach phase while reducing pilot workload and eliminating human error in energy management

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The patent replaces the manual mechanical process of pilot energy management with an automated computational system. The flight management system uses algorithms to calculate optimal vertical paths, substituting the pilot's manual evaluation and control actions with automated digital processing that continuously optimizes the descent profile based on real-time flight conditions

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Adaptability or versatility

If pilots divert from reference path for traffic control reasons, then traffic flow is managed, but multiple system interactions increase workload and complexity

Engineering Contradiction:
Improveflight path flexibilityVSAvoidsystem interaction complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The system applies dynamics by continuously adapting the vertical flight path in real-time based on changing traffic control requirements and flight conditions. When diversion from the reference path is needed, the system dynamically regenerates optimized vertical profiles that accommodate new constraints, maintaining adaptability while reducing the complexity of manual system interactions through automated recalculation

Inventive Principle:
Principle #15Dynamics

3Speed

If aircraft overshoots target point due to energy mismanagement, then the aircraft reaches the target area, but a go-around is required wasting time

Engineering Contradiction:
Improveapproach speed controlVSAvoidapproach time
Core Design Contradiction:
SpeedVSLoss of time

Solution Approach 1:

The system implements continuous feedback by monitoring aircraft energy state, position, and descent rate throughout the approach phase. The flight management system compares actual flight parameters against the optimized vertical path and automatically adjusts control commands to maintain precise energy management, ensuring the aircraft reaches the target point at the correct altitude and speed without overshooting and requiring a go-around

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent applies preliminary action by pre-calculating optimized vertical flight paths that account for energy constraints and target point requirements before the approach begins. The system proactively manages energy dissipation throughout the descent to ensure the aircraft arrives at the stabilization point with appropriate energy levels, preventing overshoot conditions before they occur

Inventive Principle:
Principle #10Preliminary action

4Productivity

If automated systems generate optimal vertical paths in real-time, then flight efficiency improves and pilot workload decreases, but computational complexity increases

Engineering Contradiction:
Improveapproach efficiencyVSAvoidcomputational system complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The system applies segmentation by dividing the vertical flight path into discrete segments or waypoints, with each segment having specific energy and altitude constraints. The flight management system computes optimized parameters for each segment independently, then integrates them into a complete vertical profile. This segmentation reduces computational complexity by breaking down the overall optimization problem into manageable sub-problems while maintaining overall approach efficiency

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS10636313B2Method and device for generating an optimum vertical path intended to be followed by an aircraft
Publication Date: 2020.04.28 AIRBUS OPERATIONS (SAS)
  • US10636313B2 patent drawing
  • US10636313B2 patent drawing

AI summary

A method and device for generating an optimum vertical path intended to be followed by an aircraft. The device comprises at least one database relating to fixed and moving obstacles, a data entering unit, a data processing unit implementing iterative processing to generate an optimum vertical path between an initial state and a final state as a function of flight strategies, that optimum vertical path being generated in such a manner as to be free of any collision with surrounding obstacles and to conform to energy constraints, and a data transmission link for transmitting that optimum vertical path to at least one user system.