3.1 - The equation of a trajectory

3.1 - The equation of a trajectory

The path of a projectile can be described without referring to time. You will derive its Cartesian equation, recover unknown launch information from points on the path, and decide which possible launches reach a target while clearing an obstacle.

Eliminating time

Can you tell whether a projectile passes through a point without first finding when it gets there? Suppose its motion from the origin is x=12tx=12t, y=16t−5t2y=16t-5t^2, with metres and seconds as units. Since t=x/12t=x/12, substitution gives

y=43x−5x2144.y=\frac43x-\frac{5x^2}{144}.

This is the path as a relation between coordinates: its Cartesian trajectory equation.

The horizontal equation is especially useful because its velocity is constant. For a launch at speed uu and angle θ\theta, with ucos⁡θ≠0u\cos\theta\ne0,

x=ucos⁡θ tt=xucos⁡θy=usin⁡θ(xucos⁡θ)−g2(xucos⁡θ)2\begin{aligned} x&=u\cos\theta\,t \\ t&=\frac{x}{u\cos\theta} \\ y&=u\sin\theta\left(\frac{x}{u\cos\theta}\right) -\frac g2\left(\frac{x}{u\cos\theta}\right)^2 \end{aligned}

Simplify the first term using sin⁡θ/cos⁡θ=tan⁡θ\sin\theta/\cos\theta=\tan\theta. In the second term, the whole time expression is squared, including its denominator.

Cartesian trajectory

With origin at launch, horizontal xx, upward yy, and nonzero horizontal launch velocity,

y=xtan⁡θ−gx22u2cos⁡2θ.y=x\tan\theta-\frac{gx^2}{2u^2\cos^2\theta}.

Equivalently, replace 1/cos⁡2θ1/\cos^2\theta by sec⁡2θ\sec^2\theta. This equation is in MF19, using VV for launch speed. You must also be able to derive it from the component equations.

For a rightward launch use ucos⁡θ>0u\cos\theta>0 and the portion x≥0x\ge0 before first impact. The complete parabola includes points that may lie outside the physical flight. A vertical launch has x=0x=0 throughout and cannot be described by dividing by its horizontal velocity.

Worked example 1: deriving a numerical path

Question. A particle is projected from OO with horizontal and upward velocity components 1212 and 16 m s−116\,\mathrm{m\,s^{-1}}. Derive its trajectory equation and find its height when x=24 mx=24\,\mathrm m, before impact. Use g=10 m s−2g=10\,\mathrm{m\,s^{-2}}.

Plan. Write both displacement equations and eliminate their common time.

x=12ty=16t−5t2t=x12y=43x−5x2144\begin{aligned} x&=12t & y&=16t-5t^2 \\ t&=\frac{x}{12} & y&=\frac43x-\frac{5x^2}{144} \end{aligned}

At x=24x=24,

y=43(24)−5(24)2144=32−20=12.y=\frac43(24)-\frac{5(24)^2}{144}=32-20=12.

Answer. The trajectory is y=4x/3−5x2/144y=4x/3-5x^2/144, and the height is 12 m12\,\mathrm m above OO.

Check. Horizontal motion gives t=24/12=2t=24/12=2. Substituting into the original vertical motion gives 16(2)−5(2)2=1216(2)-5(2)^2=12, independently confirming the point.

Change only the vertical datum. A height offset must survive the elimination of time.

Worked example 2: keeping a ground-based height

Question. The same launch takes place from a platform 6 m6\,\mathrm m above ground. Let YY be height above ground and xx the horizontal displacement from launch. Derive the trajectory and find YY at x=24 mx=24\,\mathrm m.

Plan. Include the launch height in the vertical equation before eliminating time.

x=12tY=6+16t−5t2Y=6+43x−5x2144\begin{aligned} x&=12t & Y&=6+16t-5t^2 \\ Y&=6+\frac43x-\frac{5x^2}{144} \end{aligned}

Answer. The trajectory is Y=6+4x/3−5x2/144Y=6+4x/3-5x^2/144, giving Y=18 mY=18\,\mathrm m at x=24 mx=24\,\mathrm m.

Check. At x=0x=0, the equation gives Y=6Y=6, the stated launch height. Subtracting the platform height from 1818 gives the 12 m12\,\mathrm m rise in the preceding example.

The trajectory equation predicts coordinates, while the component equations still give time and velocity. Keep both descriptions available.

Watch out

The wrong substitution t2=x2/(ucos⁡θ)t^2=x^2/(u\cos\theta) misses a square in the denominator. Correctly, t2=x2/(u2cos⁡2θ)t^2=x^2/(u^2\cos^2\theta).

Eliminate time in a fresh component model.

Unknown speed or angle

A point on the trajectory gives an equation connecting the launch speed and angle, so supplied information about one can determine the other.

With a known angle, substitute the target coordinates and solve for u2u^2, remembering that speed is positive. With known speed and unknown angle, use

sec⁡2θ=1+tan⁡2θ.\sec^2\theta=1+\tan^2\theta.

Writing p=tan⁡θp=\tan\theta turns the trajectory equation into a quadratic in pp. This is often simpler than trying inverse trigonometric functions before the algebra is finished.

Worked example 3: finding an unknown speed

Question. A particle is projected at 45∘45^\circ above the horizontal from OO and passes through (30,10)(30,10), with coordinates in metres. Find its initial speed. Use g=10 m s−2g=10\,\mathrm{m\,s^{-2}}.

Plan. Put the point and known angle into the trajectory equation, then solve for the positive speed.

Since tan⁡45∘=1\tan45^\circ=1 and cos⁡245∘=1/2\cos^245^\circ=1/2,

10=30−10(30)22u2(1/2)20=9000u2u2=450\begin{aligned} 10&=30-\frac{10(30)^2}{2u^2(1/2)} \\ 20&=\frac{9000}{u^2} \\ u^2&=450 \end{aligned}

Answer. u=152 m s−1u=15\sqrt2\,\mathrm{m\,s^{-1}}, or 21.2 m s−121.2\,\mathrm{m\,s^{-1}}.

Check. Its components are both 15 m s−115\,\mathrm{m\,s^{-1}}. It reaches x=30x=30 at t=2t=2, when y=15(2)−5(2)2=10y=15(2)-5(2)^2=10. The positive time confirms that the point is reached after launch.

Now keep the point but supply the speed instead of the angle. A second launch may satisfy exactly the same target condition.

Worked example 4: finding two possible angles

Question. A particle is projected at speed 152 m s−115\sqrt2\,\mathrm{m\,s^{-1}} and passes through (30,10)(30,10). Find the possible angles θ\theta, where 0<θ<90∘0<\theta<90^\circ, using g=10 m s−2g=10\,\mathrm{m\,s^{-2}}.

Plan. Substitute the point, put p=tan⁡θp=\tan\theta, and solve the resulting quadratic.

10=30p−10(30)22(450)(1+p2)10=30p−10(1+p2)p2−3p+2=0(p−1)(p−2)=0\begin{aligned} 10&=30p-\frac{10(30)^2}{2(450)}(1+p^2) \\ 10&=30p-10(1+p^2) \\ p^2-3p+2&=0 \\ (p-1)(p-2)&=0 \end{aligned}

Both positive roots correspond to angles in the stated interval.

Answer. θ=45∘\theta=45^\circ or θ=tan⁡−12=63.4∘\theta=\tan^{-1}2=63.4^\circ to 1 decimal place.

Check. The first launch was checked above. For tan⁡θ=2\tan\theta=2, the components are ux=310u_x=3\sqrt{10} and uy=610u_y=6\sqrt{10}, so the target time is 30/(310)=1030/(3\sqrt{10})=\sqrt{10}. Then y=610(10)−5(10)2=60−50=10y=6\sqrt{10}(\sqrt{10})-5(\sqrt{10})^2=60-50=10.

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