Aircraft Wind Estimation Device Correcting Apparent Wind Errors

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Solution Overview

Problem

Existing wind estimation methods on aircrafts are inaccurate during rotational flights due to the use of speed measurements from different points on the aircraft, leading to errors in calculating wind characteristics, and are limited to two-dimensional horizontal plane estimations.

Innovation Solution

A method that receives speed information from both the aircraft's terrestrial reference system and airspeed measurements at different points, incorporating a corrective term for apparent wind during rotational flights, allowing for three-dimensional wind vector calculations.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If wind estimation is performed using speed measurements from different points on the aircraft (ground speed at centre and air speed at front tip), then the estimation can be performed during rotational flights, but the measurement precision deteriorates due to apparent wind errors

Engineering Contradiction:
Improveapplicability during rotational flightsVSAvoidwind estimation accuracy
Core Design Contradiction:
Adaptability or versatilityVSMeasurement precision

Solution Approach 1:

The patent transforms the measurement parameters by expressing both ground speed and air speed in the same reference point (the centre of the aircraft) through mathematical coordinate transformation. This parameter change eliminates the apparent wind error caused by using measurements from different spatial locations, thereby maintaining measurement precision while enabling rotational flight estimation.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent introduces an intermediary computational step that transforms the air speed measurement from the front tip location to the centre location using the aircraft's rotational parameters. This intermediary transformation acts as a mediator that reconciles the spatial discrepancy between measurement points, allowing accurate wind estimation during rotational flights.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Ease of manufacture

If wind estimation is performed in two dimensions (horizontal plane only), then the calculation is simpler, but the adaptability is limited and cannot estimate vertical wind components

Engineering Contradiction:
Improvecalculation simplicityVSAvoidcase of use coverage
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The patent extends the wind estimation from two-dimensional (horizontal plane) to three-dimensional space by incorporating the vertical component of air speed and applying the same spatial transformation principle in all three dimensions. This dimensional extension maintains calculation systematicity while enabling comprehensive wind vector estimation including vertical components during rotational flights.

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

Data Source

PatentUS8255101B2Method and device for estimating at least one wind characteristic on an aircraft
Publication Date: 2012.08.28 AIRBUS OPERATIONS (SAS)
  • US8255101B2 patent drawing
  • US8255101B2 patent drawing
  • US8255101B2 patent drawing

AI summary

A method and a device for estimating on an aircraft at least one wind characteristic.The device (1) comprises means (7) for determining a corrective term being representative of an apparent wind created upon a rotation of the aircraft and means (4) for determining the wind characteristic taking into account such a corrective term.