Trajectory Equation (y = x tan θ − gx²/(2u² cos²θ))

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y = x tan θ − gx²/(2u² cos²θ)

What each symbol means

SymbolWhat it stands for
gg
uSpeed
xHorizontal (m)
yVertical (m)
θAngle

When to use this

Origin at launch; x horizontal; y vertical; no air.