👤 By Why Calculator Team ✔ Reviewed by Matt Le (Founder of Why Calculator) 📅 Last Updated February 14, 2026
Wind Correction Angle Calculator
Result
Wind Correction Angle (WCA): ° / rad
Adjusted Heading: ° (to stay on course)
Disclaimer: While we strive to ensure the accuracy of our calculator tools, we cannot be held responsible for any damages or financial losses resulting from their use.
Navigating through the skies with precision requires careful adjustment for wind effects. And that’s where the Wind Correction Angle calculator (WCA) becomes essential. This tool helps pilots, drone operators, and navigators adjust their aircraft’s heading to stay on course by accounting for crosswinds. It shows how to calculate the correction angle needed by looking at the desired track, true airspeed, wind speed, and wind direction.
This calculator is not just for computations; it is a practical way to ensure safer and more accurate navigation.
What is Wind Correction Angle (WCA)?
Wind Correction Angle (WCA) is the angle that a pilot or navigator must adjust the aircraft or vehicle’s heading to compensate for crosswinds, so they stay on their desired course (track).
When there’s wind coming from the side (crosswind), it pushes the aircraft off its intended track. The heading must be adjusted into the wind to counteract this effect. That angle of adjustment is the WCA.
How to Calculate Wind Correction Angle
You can calculate WCA using the following formula:
WCA = arcsin(W⋅sin(θ)/TAS)
Where:
- W = Wind speed
- θ = Wind angle = Wind direction − Desired track (in radians)
- TAS = True Airspeed
Heading Formula:
Adjusted Heading = Track + WCA
Make sure all angles are converted to radians before using trigonometric functions unless you’re using a calculator that supports degrees directly.
Example:
Suppose:
- Desired Track (course): 90° (due east)
- True Air Speed (TAS): 150 knots
- Wind Speed: 30 knots
- Wind Direction: 45° (coming from the northeast)
Step 1: Convert angles to radians:
Track = 90° = 1.5708 rad, Wind Direction = 45°
= 0.7854 rad
Step 2: Calculate wind angle θ:
θ = Wind Direction − Track = 0.7854 − 1.5708
= −0.7854 rad
Apply the WCA formula:
WCA = arcsin(30⋅sin(−0.7854) / 150)
= arcsin(30⋅(−0.7071)/150)
= arcsin(−21.2132/150) = arcsin(−0.1414) ≈−0.1420 rad
Convert to degrees:
WCA = −0.1420 × (180/π) ≈ −8.13°

This means the aircraft must turn left by 8.13° to stay on course.
Calculate Adjusted Heading:
Heading = Track + WCA = 90° − 8.13°
= 81.87°