Dynamic Aircraft Threat Controller Manager Hazard Avoidance

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Solution Overview

Problem

Current weather monitoring systems and flight planning tools lack comprehensive integration of real-time and predictive data for turbulence and icing hazards, leading to inadequate avoidance strategies for aircraft, which can result in unsafe flight conditions.

Innovation Solution

The Dynamic Aircraft Threat Controller Manager (DATCM) system processes flight plan data, weather, and atmospheric information to generate optimized flight paths that avoid areas with significant turbulence and icing by using predictive models and real-time data, providing users with interactive tools to adjust flight paths based on hazard levels.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If comprehensive hazard modeling is integrated into flight planning tools, then flight safety is improved, but device complexity increases

Engineering Contradiction:
Improveflight safetyVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system segments hazard modeling into separate functional modules: turbulence hazard assessment, icing hazard assessment, and integrated flight path optimization. Each module processes specific hazard types independently before combining results, reducing overall system complexity while maintaining comprehensive safety coverage

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent introduces an intermediary hazard assessment layer that processes raw weather data and atmospheric conditions through standardized evaluation algorithms before feeding results to the flight path planning system. This intermediary layer isolates complexity from both data sources and decision-making systems

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If real-time and predictive weather data are processed, then hazard avoidance capability is improved, but use of energy increases

Engineering Contradiction:
Improvehazard avoidance capabilityVSAvoidenergy consumption
Core Design Contradiction:
ReliabilityVSUse of energy by moving object

Solution Approach 1:

The system implements periodic data processing cycles where weather and atmospheric data are updated at predetermined time intervals rather than continuously. The processor alternates between active hazard assessment periods and lower-power states, maintaining safety monitoring while reducing overall energy consumption

Inventive Principle:
Principle #19Periodic action

Solution Approach 2:

The patent applies partial processing by focusing computational resources on only those flight path segments where hazard conditions are detected or predicted. Rather than processing entire flight paths uniformly, the system selectively intensifies analysis only in hazardous regions, reducing total energy usage

Inventive Principle:
Principle #16Partial or excessive action

3Productivity

If optimized flight paths are generated to avoid hazards, then flight efficiency is improved, but device complexity increases

Engineering Contradiction:
Improveflight efficiencyVSAvoidsystem complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The flight path optimization system dynamically adjusts routing based on real-time hazard assessments rather than using static predetermined paths. The system continuously evaluates multiple potential routes and adapts the optimal path as hazard conditions change, improving flight efficiency through responsive adaptation

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The patent implements preliminary hazard assessment and flight path planning before actual flight operations. By pre-processing weather data and identifying hazardous regions in advance, the system establishes optimized flight paths proactively, reducing the need for complex real-time decision-making during flight

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS11183074B2Dynamic aircraft threat controller manager apparatuses, methods and systems
Publication Date: 2021.11.23 DTN LLC
  • US11183074B2 patent drawing
  • US11183074B2 patent drawing
  • US11183074B2 patent drawing

AI summary

The DYNAMIC AIRCRAFT THREAT CONTROLLER MANAGER APPARATUSES, METHODS AND SYSTEMS (“DATCM”) transforms flight profile information, terrain, weather/atmospheric data and flight parameter data via DATCM components into comprehensive hazard avoidance optimized flight plans. Comprehensive hazard avoidance includes synergistic comprehensive turbulence and airfoil-specific icing data. In one implementation, the DATCM comprises a processor and a memory disposed in communication with the processor and storing processor-issuable instructions to receive anticipated flight plan parameter data, obtain weather data based on the flight plan parameter data, obtain atmospheric data based on the flight plan parameter data, and determine a plurality of four-dimensional grid points based on the flight plan parameter data. The DATCM may then determine comprehensive hazards mappings. With (near) real-time comprehensive hazard information and/or predictive turbulence/icing forecast specific to airfoil type and/or profile parameters, the DATCM may allow aircraft to avoid areas where comprehensive hazard is greater than a predetermined threshold and/or avoid areas where turbulence/icing may occur.