UAV Wind Estimation via Constant Bank Angle Turns

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Solution Overview

Problem

Unmanned aerial vehicles (UAVs) face challenges in accurately determining wind conditions without external equipment, leading to deviations from intended flight paths and increased resource usage when attempting to identify wind information, which affects their mission objectives and range.

Innovation Solution

The method involves flying the UAV at a constant bank angle to cross the intended ground track, using position data to identify wind speed and direction, and adjusting the heading to maintain the intended path without repeated course corrections, utilizing onboard sensors and data processing to calculate wind information.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of information

If weather balloons are used to obtain wind information, then wind data can be obtained, but the cost and time increase

Engineering Contradiction:
Improvewind informationVSAvoidtime to obtain wind data
Core Design Contradiction:
Loss of informationVSLoss of time

Solution Approach 1:

The aircraft performs constant bank angle turns to autonomously determine wind direction and strength using its own motion data and onboard sensors, eliminating the need for external weather balloon data or air traffic control wind information services

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system proactively performs wind determination maneuvers during flight operations to obtain wind information before it is needed for course correction, rather than relying on delayed weather balloon data or requesting it from external sources

Inventive Principle:
Principle #10Preliminary action

2Loss of information

If weather balloons are used to obtain wind information, then wind data can be obtained, but the cost increases

Engineering Contradiction:
Improvewind informationVSAvoidcost to obtain wind data
Core Design Contradiction:
Loss of informationVSLoss of energy

Solution Approach 1:

The aircraft uses its own constant bank angle turn maneuvers and onboard position sensors to self-determine wind conditions, eliminating the need to purchase or access expensive weather balloon data from external providers

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system uses inexpensive onboard position sensors and the aircraft's own motion to determine wind information, replacing expensive external weather observation infrastructure with low-cost self-contained measurement

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

3Loss of information

If hardware to receive wind information from air traffic control is installed, then wind data can be obtained, but payload restrictions are violated

Engineering Contradiction:
Improvewind informationVSAvoidpayload weight
Core Design Contradiction:
Loss of informationVSWeight of moving object

Solution Approach 1:

The aircraft determines wind information autonomously using its own constant bank angle turn maneuvers and existing onboard position sensors, eliminating the need for additional wind reception hardware that would increase payload weight

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system uses the aircraft's existing position sensors and flight control capabilities for multiple purposes: normal navigation and wind determination, eliminating the need for dedicated wind information reception hardware

Inventive Principle:
Principle #6Universality (Multi-functionality)

4Ease of operation

If the aircraft does not account for cross wind, then the flight path is simple, but the aircraft drifts off course

Engineering Contradiction:
Improveflight path controlVSAvoidground track accuracy
Core Design Contradiction:
Ease of operationVSMeasurement precision

Solution Approach 1:

The system uses the aircraft's position data during constant bank angle turns to calculate wind direction and strength, then applies this feedback information to adjust the heading and maintain accurate ground track despite crosswind conditions

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system determines wind information through constant bank angle turns before using it for course correction, proactively preparing the wind data needed for accurate navigation rather than reacting to drift after it occurs

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentEP3410249B1System to estimate wind direction and strength using constant bank angle turn
Publication Date: 2020.12.02 THE BOEING CO
  • EP3410249B1 patent drawingFigure 1
  • EP3410249B1 patent drawingFigure 2
  • EP3410249B1 patent drawingFigure 3

AI summary

Information is identified about a wind using positions of an aircraft flying along a maneuver ground track at a constant bank angle which crosses an intended ground track of the aircraft.