Aircraft Holding Control by Flight Mode for Congested Airports

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Solution Overview

Problem

Existing aircraft control technologies do not consider energy efficiency when aircraft hold over airports, leading to inefficiencies in energy consumption.

Innovation Solution

An information processing apparatus that communicates with aircraft to determine their flight mode and instructs them to use either fixed wing or vertical flight modes based on airport congestion and weather conditions, optimizing energy usage.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Use of energy by moving object

If aircraft hold over congested airport using conventional control methods, then aircraft can maintain position and wait for landing clearance, but energy consumption increases due to lack of optimization for different aircraft types

Engineering Contradiction:
Improveenergy efficiencyVSAvoidcontrol system complexity
Core Design Contradiction:
Use of energy by moving objectVSDevice complexity

Solution Approach 1:

The patent applies parameter changes by adjusting holding patterns and procedures based on aircraft type parameters. The system changes control parameters (holding pattern type, altitude, duration) according to the specific aircraft configuration (fixed-wing vs. rotary-wing) to optimize energy efficiency while maintaining safety and operational effectiveness.

Inventive Principle:
Principle #35Parameter changes

2Ease of manufacture

If uniform holding instructions are given to all aircraft types, then control procedures are simplified, but energy efficiency deteriorates because different aircraft types have different optimal holding methods

Engineering Contradiction:
Improvecontrol procedure simplicityVSAvoidenergy consumption
Core Design Contradiction:
Ease of manufactureVSUse of energy by moving object

Solution Approach 1:

The patent applies local quality by providing differentiated holding instructions tailored to specific aircraft types rather than uniform instructions for all. The control system assigns different holding patterns, altitudes, and procedures based on the local characteristics of each aircraft type (fixed-wing vs. rotary-wing), optimizing energy efficiency for each specific case.

Inventive Principle:
Principle #3Local quality

3Ease of operation

If aircraft use vertical flight mode for holding, then maneuverability is improved for rotary-wing aircraft, but energy consumption increases compared to fixed-wing mode

Engineering Contradiction:
ImprovemaneuverabilityVSAvoidpower consumption
Core Design Contradiction:
Ease of operationVSUse of energy by moving object

Solution Approach 1:

The patent applies dynamics by allowing aircraft to dynamically switch between different flight modes (vertical flight, fixed-wing flight, holding patterns) based on operational requirements and energy efficiency considerations. The system optimizes the balance between maneuverability and power consumption by selecting appropriate flight modes for different phases of operation.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS20250292692A1Information processing apparatus, aircraft control method, and method for improving travel maas
Publication Date: 2025.09.18 TOYOTA JIDOSHA KK
  • US20250292692A1 patent drawing
  • US20250292692A1 patent drawing
  • US20250292692A1 patent drawing

AI summary

An information processing apparatus includes a controller, and the controller is configured to acquire body information indicating whether an aircraft has a fixed wing mode from the aircraft in a case in which an airport is congested and the aircraft is about to land at the airport, and notify the aircraft of an instruction to hold in air using the fixed wing mode in a case in which the aircraft has the fixed wing mode, and notify the aircraft of an instruction to hold in air using a vertical flight mode in a case in which the aircraft does not have the fixed wing mode.