Crosswind Calculator — Method, Assumptions, and Quick Checks
I am Aidan Mercer, Physics Analyst & Calculator Designer. This calculator resolves wind into components relative to a runway: crosswind (signed, right positive) and head/tailwind (headwind positive). SI or aviation units can be used; internal math is unit-agnostic when angles are consistent.
Variables and Units
- Wind speed V: magnitude of the ambient wind (kt, mph, km/h, m/s). Nonnegative.
- Wind direction W (deg): meteorological “from” direction, 0–360°.
- Runway heading R (deg): runway magnetic/true course used for takeoff/landing, 0–360°. Use the same reference as W.
Formulas (per spec)
- Angle difference (signed, −180° to +180°): angleDiff = ((W − R + 540) % 360) − 180
- Crosswind component: crosswind = V·sin(angleDiff·degToRad)
- Head/tailwind component: headwind = V·cos(angleDiff·degToRad)
- Absolute crosswind: crosswindAbs = |crosswind|
Sign conventions: crosswind > 0 means wind from the right; headwind > 0 means headwind, headwind < 0 indicates tailwind.
Assumptions and Scope
- Flat-earth, steady wind; instantaneous components relative to a single runway heading.
- Angles follow aviation convention: directions in degrees, wind as “from”.
- No Coriolis or gust modeling; ignores terrain/obstruction effects.
- Headings must share the same reference (both magnetic or both true).
Input Constraints and Edge Cases
- Wind speed V ≥ 0. If V = 0, all components are 0.
- Angles can be any real number; they are wrapped into 0–360° before computing.
- At angleDiff ≈ ±90°, headwind ≈ 0 (pure crosswind).
- At angleDiff ≈ 0°, crosswind ≈ 0 (pure headwind).
Worked Example (matches spec)
Given: V = 12 kt, W = 240°, R = 210°.
- angleDiff = ((240 − 210 + 540) % 360) − 180 = 30°
- crosswind = 12·sin(30°) = 6 kt (from right)
- headwind = 12·cos(30°) ≈ 10.3923 kt (headwind)
- crosswindAbs = 6 kt
Units and Conversion Notes
- Use consistent speed units; angles always in degrees in the UI (internally converted to radians).
- Changing units scales both components identically; signs unaffected.
Uncertainty and Sensitivity
- First-order propagation: δcrosswind ≈ |sin θ|·δV + |V·cos θ|·degToRad·δθ; δheadwind ≈ |cos θ|·δV + |V·sin θ|·degToRad·δθ, where θ = angleDiff.
- Near θ = 90°, headwind is sensitive to small angle errors; near θ = 0°, crosswind is sensitive.
Sanity Checks
- W = R → crosswind = 0, headwind = +V.
- W = R ± 90° → headwind = 0, crosswind = ±V (sign indicates left/right).
- V = 0 → all outputs 0.