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Projectile model: acceleration components and notation
FORMULA
ax=0
ay=−g
DERIVATION
Only weight acts during free flight.
Use Newton's second law horizontally.
Fx=max=0⇒ax=0
Fy=may=−mg⇒ay=−g
ASSUMPTIONS
No air resistance. Constant g. Launch is at (0, 0). Angled launches use 0 < θ < 90° unless stated otherwise.
SYMBOLS
u = launch speed
θ = launch angle above the horizontal
t = time since launch
x = horizontal displacement
y = vertical displacement above launch
g = positive gravitational acceleration
H = maximum rise above launch
T = total flight time
R = horizontal range
h = positive drop to the landing level
FORMULA
ux=ucosθ
uy=usinθ
DERIVATION
Draw a right-angled velocity triangle. The hypotenuse is the launch speed u.
Use the cosine ratio for the horizontal component.
cosθ=uux
ux=ucosθ
sinθ=uuy
uy=usinθ
CHECK
The component squares add to the square of the launch speed.
FORMULA
vx=ucosθ
DERIVATION
vx=ux+axt
vx=ucosθ+0t
vx=ucosθ
WHAT IT MEANS
Horizontal velocity stays constant throughout free flight.
FORMULA
vy=usinθ−gt
DERIVATION
vy=uy+ayt
uy=usinθ,ay=−g
vy=usinθ−gt
WHAT IT MEANS
Vertical velocity is positive on ascent, zero at the peak and negative on descent.
FORMULA
x=(ucosθ)t
DERIVATION
x=uxt+21axt2
x=(ucosθ)t+21(0)t2
x=(ucosθ)t
t=ucosθx
REMEMBER
Use this same time in the vertical equations. The rearrangement requires a nonzero horizontal velocity.
FORMULA
y=(usinθ)t−21gt2
DERIVATION
y=uyt+21ayt2
uy=usinθ,ay=−g
y=(usinθ)t−21gt2
SIGN CHECK
y is measured from launch. A landing h below launch has y = −h. If launch is h above ground, height above ground is h + y.
FORMULA
vy2=u2sin2θ−2gy
DERIVATION
vy2=uy2+2ayy
vy2=(usinθ)2+2(−g)y
vy2=u2sin2θ−2gy
REMEMBER
This gives the vertical component, not the total speed. Squaring loses the direction, so choose rising or falling separately.
FORMULA
y=xtanθ−2u2cos2θgx2
DERIVATION
t=ucosθx
y=(usinθ)(ucosθx)−2g(ucosθx)2
y=cosθxsinθ−2u2cos2θgx2
cosθsinθ=tanθ
WHAT IT MEANS
The path is a downward-opening parabola. The equation requires nonzero horizontal velocity.
FRACTION CHECK
Only the second term is subtracted as a fraction. Its whole numerator is gx² and its whole denominator is 2u² cos²θ.
FORMULA
tpeak=gusinθ
DERIVATION
vy=0
0=usinθ−gtpeak
gtpeak=usinθ
tpeak=gusinθ
WHEN TO USE IT
An upward launch that reaches its peak before a collision.
REMEMBER
Vertical velocity is zero at the peak. Acceleration is still −g.
FORMULA
H=2gu2sin2θ
DERIVATION
vy=0,y=H
vy2=uy2+2ayy
0=(usinθ)2−2gH
2gH=u2sin2θ
H=2gu2sin2θ
WHEN TO USE IT
An upward launch that reaches its peak before a collision.
REMEMBER
H is the rise above launch. Add the launch height to get maximum height above ground.
FORMULA
xpeak=gu2sinθcosθ
xpeak=2gu2sin(2θ)
DERIVATION
tpeak=gusinθ
xpeak=(ucosθ)(gusinθ)
xpeak=gu2sinθcosθ
2sinθcosθ=sin(2θ)
WHEN TO USE IT
The projectile must reach its peak before a collision.
SAME-HEIGHT LANDING
The highest point is halfway across the range: x at the peak = R/2.
FORMULA
vmin=ucosθ
DERIVATION
v2=vx2+vy2
vy=0⇒vmin2=vx2
vmin=u2cos2θ=ucosθ
WHEN TO USE IT
An upward launch with positive horizontal velocity that reaches its peak.
REMEMBER
Only the vertical velocity is zero there. The projectile is still moving horizontally.
FORMULA
T=g2usinθ
DERIVATION
y=0
0=(usinθ)T−21gT2
0=T(usinθ−21gT)
usinθ−21gT=0
T=g2usinθ
WHEN TO USE IT
Launch and landing must be at the same height.
REMEMBER
The total flight time is twice the time to the peak. Ascent and descent take equal times.
FORMULA
sin(2θ)=2sinθcosθ
DERIVATION
sin(A+B)=sinAcosB+cosAsinB
sin(θ+θ)=sinθcosθ+cosθsinθ
sin(2θ)=2sinθcosθ
WHY IT IS USEFUL
It makes the horizontal range equation shorter.
FORMULA
R=gu2sin(2θ)
DERIVATION
R=(ucosθ)T
T=g2usinθ
R=(ucosθ)(g2usinθ)
R=g2u2sinθcosθ
R=gu2sin(2θ)
WHEN TO USE IT
Launch and landing must be at the same height.
REMEMBER
R is horizontal distance. It is not the length of the curved flight path.
FORMULA
θ=45∘
Rmax=gu2
DERIVATION
R=gu2sin(2θ)
sin(2θ)=1
2θ=90∘⇒θ=45∘
Rmax=gu2
WHEN TO USE IT
Fixed launch speed and equal launch and landing heights. For unequal heights, 45° is generally not the best angle.
FORMULA
R(θ)=R(90∘−θ)
DERIVATION
R(θ)=gu2sin(2θ)
R(90∘−θ)=gu2sin(180∘−2θ)
sin(180∘−A)=sinA
R(90∘−θ)=gu2sin(2θ)=R(θ)
WHEN TO USE IT
Same launch speed, same g and both land at launch height.
REMEMBER
The larger launch angle gives a greater maximum height and a longer flight time.
FORMULA
H=8gT2
DERIVATION
T=g2usinθ⇒usinθ=2gT
H=2g(usinθ)2
H=2g(2gT)2
H=8gg2T2=8gT2
WHEN TO USE IT
T is the whole flight time back to launch height, not just the time to the peak.
FORMULA
H=4Rtanθ
DERIVATION
H=2gu2sin2θ
R=g2u2sinθcosθ
RH=2gu2sin2θ×2u2sinθcosθg
RH=4cosθsinθ=4tanθ
H=4Rtanθ
WHEN TO USE IT
Equal launch and landing heights, with 0 < θ < 90°.
FORMULA
v=(ucosθ)2+(usinθ−gt)2
DERIVATION
v2=vx2+vy2
v2=(ucosθ)2+(usinθ−gt)2
v=(ucosθ)2+(usinθ−gt)2
OPTIONAL EXPANSION
The same result can be written as v² = u² − 2ugt sinθ + g²t².
FORMULA
v2=u2−2gy
v=u2−2gy
DERIVATION
vy2=u2sin2θ−2gy
vx2=u2cos2θ
v2=u2(cos2θ+sin2θ)−2gy
cos2θ+sin2θ=1
v2=u2−2gy
CONSEQUENCES
Speed is u again at launch height. At a drop h below launch, y = −h and v² = u² + 2gh. The projectile must actually reach the chosen height.
FORMULA
tanϕ=ucosθusinθ−gt
ϕ=tan−1(ucosθusinθ−gt)
DERIVATION
tanϕ=vxvy
tanϕ=ucosθusinθ−gt
ϕ=tan−1(ucosθusinθ−gt)
WHEN TO USE IT
The horizontal velocity is positive, as in this set.
REMEMBER
Positive φ means rising. Zero means the peak. Negative φ means falling.
FORMULA
t=gusinθ±u2sin2θ−2gY
DERIVATION
Y=(usinθ)t−21gt2
21gt2−(usinθ)t+Y=0
t=2A−B±B2−4AC
A=2g,B=−usinθ,C=Y
t=gusinθ±u2sin2θ−2gY
INTERPRETING THE ANSWERS
For a height between launch and the peak, the minus root is on ascent and the plus root is on descent. At the peak they coincide. A negative discriminant means the height cannot be reached. Keep only nonnegative times before a collision.
FORMULA
T=gusinθ+u2sin2θ+2gh
DERIVATION
−h=(usinθ)T−21gT2
21gT2−(usinθ)T−h=0
T=gusinθ±u2sin2θ+2gh
T=gusinθ+u2sin2θ+2gh
CHECK
For an upward launch, setting h = 0 recovers the same-height flight time.
FRACTION CHECK
The entire sum, including the square root, is divided by g.
FORMULA
R=gucosθ(usinθ+u2sin2θ+2gh)
DERIVATION
R=(ucosθ)T
T=gusinθ+u2sin2θ+2gh
R=(ucosθ)(gusinθ+u2sin2θ+2gh)
R=gucosθ(usinθ+u2sin2θ+2gh)
WHEN TO USE IT
h is a positive drop to a horizontal landing level.
CHECK
For an upward launch, h = 0 gives the same-height range equation.
FORMULA
T=g2h
DERIVATION
uy=0,ay=g
h=0T+21gT2
T2=g2h
T=g2h
WHEN TO USE IT
Horizontal launch, landing h below launch.
SQUARE-ROOT CHECK
Both 2h and g are inside the square root.
WHAT IT MEANS
For a fixed h, flight time does not depend on the horizontal launch speed.
FORMULA
R=ug2h
DERIVATION
vx=u
T=g2h
R=uT
R=ug2h
WHEN TO USE IT
Horizontal launch, landing h below launch.
SQUARE-ROOT CHECK
The launch speed u is outside the square root. The whole fraction 2h/g is inside it.
FORMULA
y=−2u2gx2
DERIVATION
x=ut⇒t=ux
y=−21gt2
y=−2g(ux)2
y=−2u2gx2
SIGN CHECK
y is measured upwards from launch, so it is negative below launch. A positive downward drop d instead satisfies d = −y.
FORMULA
v=u2+2gh
DERIVATION
vx=u
vy2=02+2gh=2gh
v2=vx2+vy2=u2+2gh
v=u2+2gh
WHEN TO USE IT
Horizontal launch, landing h below launch.
SQUARE-ROOT CHECK
The whole sum u² + 2gh is inside the square root.
FORMULA
d=21gt2
d=2u2cos2θgx2
DERIVATION
y0=(usinθ)t
y=(usinθ)t−21gt2
d=y0−y=21gt2
t=ucosθx
d=2g(ucosθx)2=2u2cos2θgx2
REMEMBER
d is measured vertically below the initial straight-line direction, not perpendicular to that line. It is not generally the height lost since launch