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Correction Angle

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on
Jun 26, 2024, 1:38:33 PM
Created by
on
Apr 26, 2014, 12:53:06 PM
` = Delta(vec( alpha ^o & "AS" ) , vec( beta ^o & "WS" ))`
`(AS)"Air Speed"`
`(alpha)"Flight Direction"`
`(WS)"Wind Speed"`
`(beta)"Wind Direction"`
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b67b4c17-cd41-11e3-b7aa-bc764e2038f2

The Flight Navigation Correction Angle calculator computes the navigation angle/azimuth correction angle (Δ) using the wind speed (WS), wind direction (β), Flight Heading (α) and an Air Speed (AS). 
/attachments/b67b4c17-cd41-11e3-b7aa-bc764e2038f2/CorrectionAngle-illustration.pngCorrection angle parameters

INSTRUCTIONS: Choose units and enter the following:

  • (α) Flight Angle(azimuth)
  • (AS) Air Speed
  • (WS) Wind Speed
  • (β) Wind Direction

Navigation Correction Angle (Δ):  The calculator returns the angle in degrees.  However this can be automatically converted to compatible units via the pull-down menu.


Flight and Navigation Calculators

  • Correction AngleComputes the navigation angle/azimuth correction angle using the wind speed, wind direction, flight heading and an Air Speed.
  • Ground SpeedComputes the ground speed based on the wind speed, wind direction, a Flight Heading and an Air Speed.
  • Haversine - DistanceComputes the distance between two points on a spherical model of the Earth along a great circle arc.  This also includes the rhumb line distance and azimuth for the rhumb line.
  • Travel Time between CoordinatesComputes the time to travel between to points on the globe in a great circle arc at an average velocity. 
  • Distance to Sea Level Horizon at Altitude: Computes the distance to the horizon from a specified height using a spherical model the mean spherical radius of the Earth
  • Force of Drag: Calculates the resisting force of drag on an object flowing through a medium (e.g. air).
  • Force of Lift: Computes the lifting force on the surface area of a wing based on the wing surface area, air flow velocity, density of air and a lift coefficient.
  • Lift Coefficient: Compute the lift coefficient of a wing based on lift force, wing surface area, wind speed and density of air.
  • Velocity Needed for Takeoff: Computes the velocity required to create more lift than the weight of an aircraft or watercraft using a wing (e.g. hydrofoil).
  • Glide Ratio: Computes the glide ratio based on the change in forward distance and the change in altitude.
  • Wing Surface Area: Computes the wing surface area required to achieve lift, base on a lift coefficient, lift force, wind speed and density of air.
  • Velocity of Air over the Wing: Computes the velocity required to achieve a lift, based on lift coefficient, lift force, wing surface area and density of air.
  • Air Speed from Pressures: It uses the Bernoulli Equation to estimate air speed based on the total Pressure measured by a pilot tube, total Static local atmospheric pressure and the Density of Air.
  • Center of Mass: Computes the vehicle center of mass between two loads (masses).


Sailing and Navigation Calculators:

The Math / Science

The Navigation Correction Angle formula calculate the course correction angle needed to compensate for wind of a certain bearing and at a certain velocity in order to continue at the desired heading.  This is done with vector arithmetic.  


This equation, Correction Angle, is used in 4 pages
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on
Aug 20, 2014 01:54 PM
Excellent equation.

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