Rotorcraft landing device

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Solution Overview

Problem

Rotorcrafts equipped with cameras for landing pose privacy concerns due to their ability to capture surrounding environments, necessitating a solution for rotorcrafts without image capturing functions to land safely and efficiently.

Innovation Solution

A rotorcraft landing device with a landing portion, position recognition mechanism, and remote control system that allows rotorcrafts without image capturing functions to land by using image capturing portions, distance measuring, and movable members for accurate positioning and control.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Extent of automation

If a rotorcraft is equipped with an image capturing function for automatic landing, then the landing precision and automation level are improved, but the privacy protection and portrait right protection deteriorate

Engineering Contradiction:
Improveautomatic landing capabilityVSAvoidprivacy infringement
Core Design Contradiction:
Extent of automationVSObject-affected harmful factors

Solution Approach 1:

The image capturing function is extracted and removed from the rotorcraft system. The patent explicitly states that the rotorcraft is designed without any image capturing devices, thereby eliminating the source of privacy infringement while maintaining landing capability through alternative means

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

A ground-based position recognition system acts as an intermediary between the rotorcraft and the landing location. The system uses multiple cameras positioned on the ground to track and recognize the rotorcraft's position, allowing automatic landing control without requiring cameras on the rotorcraft itself

Inventive Principle:
Principle #24Intermediary (Mediator)

2Object-affected harmful factors

If a rotorcraft without image capturing function is used to protect privacy, then the privacy protection is improved, but the landing control capability and positioning accuracy deteriorate

Engineering Contradiction:
Improveprivacy protectionVSAvoidposition recognition accuracy
Core Design Contradiction:
Object-affected harmful factorsVSMeasurement precision

Solution Approach 1:

Multiple ground-based cameras are merged into a coordinated system that works together to track the rotorcraft from different angles and positions. This combination of multiple sensing elements compensates for the absence of onboard cameras and achieves accurate position recognition

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The position recognition system transitions from a single-point onboard camera to a multi-point ground-based camera network, adding spatial dimensions to the observation. This dimensional change allows the system to track the rotorcraft's position and orientation through geometric calculations based on multiple viewing angles

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

3Measurement precision

If multiple image capturing portions are deployed for accurate position recognition, then the positioning precision is improved, but the device complexity and cost increase

Engineering Contradiction:
Improveposition recognition precisionVSAvoidsystem complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The ground-based camera system uses the rotorcraft's own reflected light and natural environmental lighting to create recognizable images, without requiring additional active markers or complex retro-reflective materials on the rotorcraft. The system processes the rotorcraft's visual features directly as they appear in the natural environment

Inventive Principle:
Principle #25Self-service

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

Enables secure and efficient landing of rotorcrafts without image capturing functions, protecting privacy and facilitating landing in environments with limited GPS signals, while ensuring safe package delivery and operation in various weather conditions.

Implementation Method 1

the position recognition portion may be configured to include image capturing portions provided at a plurality of positions on the landing portion, and recognize the position of the rotorcraft with respect to the landing portion on a basis of a result of image capturing performed by the image capturing portions

Methodology Applied
Scientific EffectImage capturing: Photography

Implementation Method 2

a distance measuring portion that measures a distance from the landing portion to the rotorcraft

Methodology Applied
Scientific EffectDistance measurement: LIDAR

Data Source

PatentUS11747829B2Rotorcraft landing device
Publication Date: 2023.09.05 AERONEXT INC
  • US11747829B2 patent drawing
  • US11747829B2 patent drawing
  • US11747829B2 patent drawing

AI summary

A drone loaded with a package takes off from a takeoff device and uses a GPS system to fly to a user house that is a delivery destination of the package as the destination. Further, when the drone approaches the user house that is the destination, the flight of the drones is switched from autonomous navigation using the GPS system to remote control performed by a landing device and an in-house control device installed in the user house. The drone lands on the landing device by remote control from the landing device and the in-house control device, separates the package, and then returns to the warehouse using the GPS system and lands on the takeoff device.