UAV Landing Guidance Using Airdrome Position Detectors

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Solution Overview

Problem

Existing unmanned aerial vehicle (UAV) landing systems face challenges due to GPS data drift, leading to inaccurate landings and increased operational costs, as manual updates are labor-intensive and prone to errors.

Innovation Solution

An airdrome auxiliary positioning system that uses multiple position detectors to determine the UAV's location over a target airdrome, generates correction guidance information based on the offset vector between the actual and target locations, and sends this information to the UAV to guide it into the signal coverage of a guidance beacon for precise landing.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If manual updates are used to correct GPS data drift, then positioning accuracy can be improved, but labor intensity and operational costs increase

Engineering Contradiction:
Improvepositioning accuracyVSAvoidlabor intensity
Core Design Contradiction:
Measurement precisionVSEase of operation

Solution Approach 1:

The system uses the UAV's own transmitted signal as the measurement target for position detectors, enabling automatic positioning correction without manual intervention. The UAV serves itself as both the signal source and the measurement object, eliminating the need for manual GPS updates.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The patent replaces manual mechanical operations with an automated electronic system. Position detectors automatically measure the UAV's position by analyzing its transmitted signal, and the system automatically generates correction guidance information, substituting manual labor with automated detection and processing.

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

2Manufacturing precision

If extensive manual updates are performed to maintain positioning accuracy, then landing precision improves, but time consumption and operational complexity increase

Engineering Contradiction:
Improvelanding precisionVSAvoidtime consumption
Core Design Contradiction:
Manufacturing precisionVSLoss of time

Solution Approach 1:

The system continuously tracks the UAV's position by constantly measuring its transmitted signal during flight. This continuous automatic measurement and correction process maintains landing precision throughout the entire flight without requiring intermittent manual updates, saving time and reducing operational complexity.

Inventive Principle:
Principle #20Continuity of useful action

Solution Approach 2:

The patent introduces position detectors as an intermediary between the UAV and the control system. These detectors automatically measure the UAV's position by receiving its signal and generate correction guidance information, eliminating the need for manual measurement and update operations.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Device complexity

If GPS data is used without correction, then system simplicity is maintained, but positioning accuracy and landing reliability deteriorate

Engineering Contradiction:
Improvesystem simplicityVSAvoidlanding reliability
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The patent introduces position detectors as an intermediary component that automatically measures the UAV's position and generates correction guidance information. This intermediary system bridges the gap between the simple GPS and the control system, improving reliability without requiring complex manual intervention procedures.

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS12307913B2Method and system for guiding landing of unmanned aerial vehicle, auxiliary positioning system, and unmanned aerial vehicle
Publication Date: 2025.05.20 BEIJING SANKUAI ONLINE TECH CO LTD
  • US12307913B2 patent drawing
  • US12307913B2 patent drawing
  • US12307913B2 patent drawing

AI summary

The disclosure relates to a method for guiding landing of an unmanned aerial vehicle. The method for guiding landing of unmanned aerial vehicle includes: determining location information of the unmanned aerial vehicle over a target airdrome by using a plurality of position detectors in an airdrome auxiliary positioning system; generating correction guidance information according to an offset vector between the location information and target location information, where the target location information is information representing any location within signal coverage of a guidance beacon of the target airdrome; and sending the correction guidance information to the unmanned aerial vehicle, where the correction guidance information is used to guide the unmanned aerial vehicle to fly into the signal coverage of the guidance beacon.