Wind Correction Angle Calculator

Find the wind correction angle (crab angle), true heading, ground speed, and crosswind component from true airspeed, wind speed, wind direction, and your desired true course.

Quick Facts

Wind correction angle
WCA = arcsin[(Wind Speed ÷ TAS) × sin(Wind Angle)]
Wind angle is the difference between the wind's FROM direction and your desired true course.
Heading to fly
Heading = True Course + WCA
Add WCA when the wind comes from the right of course; subtract when it comes from the left.
Ground speed
GS = TAS × cos(WCA) − Wind Speed × cos(Wind Angle)
Headwind components reduce ground speed; tailwind components increase it.

Your Results

Calculated
Wind Correction Angle
-
Degrees left or right of course
True Heading to Fly
-
Course corrected for wind drift
Ground Speed
-
Actual speed over the ground
Crosswind Component
-
Wind perpendicular to your course

Ready

Enter airspeed, wind, and course data, then press Calculate.

Formula and Method for Wind Correction Angle

When an aircraft flies through moving air, the wind pushes it sideways off the intended path. The wind correction angle (WCA), also called the crab angle, is the number of degrees a pilot offsets the aircraft's nose from the desired true course so that the combination of airspeed and wind produces a ground track that matches the plan. This calculator solves the classic dead-reckoning "wind triangle" — the same relationship taught for E6B flight computers — using true airspeed, wind speed, wind direction, and true course.

How the calculation works

First, the wind angle is found as the difference between the wind's FROM direction and the true course, normalized to between -180° and 180°. The wind correction angle is then WCA = arcsin[(Wind Speed ÷ True Airspeed) × sin(Wind Angle)]. A positive wind angle (wind from the right of course) gives a positive WCA, meaning turn right; a negative wind angle (wind from the left) gives a negative WCA, meaning turn left. The heading to fly is simply Heading = True Course + WCA. Ground speed follows from the same triangle: GS = TAS × cos(WCA) − Wind Speed × cos(Wind Angle), where a headwind component (wind angle near 0°) subtracts from ground speed and a tailwind component (wind angle near 180°) adds to it.

Common mistakes

  • Confusing "wind FROM" with "wind TO": aviation wind direction is always reported as the direction the wind is blowing from, not the direction it is blowing toward — mixing these up flips the correction to the wrong side.
  • Ignoring the crosswind limit: if the crosswind component (Wind Speed × sin(Wind Angle)) exceeds true airspeed, the arcsin has no real solution — no heading can hold that course, and the calculator will flag it as invalid.
  • Mixing true and magnetic values: true course and wind direction must use the same reference (true north); mixing in a magnetic heading without applying variation introduces a systematic error.

Real-world applications

  • VFR and IFR flight planning use WCA to compute the heading a pilot should fly to track a course line accurately between waypoints.
  • Glider and sailplane pilots use the same wind triangle to plan cross-country legs where drift can significantly affect range.
  • Marine navigators solve an equivalent "current triangle" to correct a vessel's heading for water current instead of wind.
  • Long-range drone and UAV mission planning uses wind correction to keep autonomous routes on their programmed ground track.

Frequently Asked Questions

What is a wind correction angle (WCA)?
The wind correction angle, also called the crab angle, is the number of degrees a pilot points the aircraft's nose left or right of the desired course to counteract crosswind drift, so the aircraft's actual path over the ground matches the intended true course.
What is the formula for wind correction angle?
WCA = arcsin[(Wind Speed / True Airspeed) × sin(Wind Angle)], where the wind angle is the difference between the wind's FROM direction and the desired true course. Add the result to the course to correct right, or subtract it to correct left, depending on which side the wind is coming from.
What happens if the crosswind component is greater than the true airspeed?
There is no valid heading. The formula requires (Wind Speed × sin(Wind Angle)) / True Airspeed to stay between -1 and 1; if the crosswind exceeds true airspeed, the aircraft cannot generate enough sideways component to hold the course, and the flight must accept drift, wait for calmer wind, or choose a different route.
How is ground speed related to wind correction angle?
Once WCA is known, ground speed is GS = TAS × cos(WCA) − Wind Speed × cos(Wind Angle). A headwind component reduces ground speed and a tailwind component increases it, on top of the small speed loss caused by crabbing into the wind.