Projectile Motion Analyzed — Question 7

Section 4-5 · Physics pages 544–545

Question 7 Minimize launch speed by choosing the flight time A point target is at (12, 5) m relative to launch. You may choose any positive arrival time T and launch direction. Neglect air resistance and use uniform g = 10 m/s2 downward. Unless stated otherwise, x is horizontal and y upward. For this task minimize the initial speed; there are no obstacles. x y target Schematic optimum trajectory to an elevated target; the initial tangent is steeper than the line of sight. (a) Express the required launch velocity components and squared speed as functions of T. (b) Find the minimum speed and the corresponding arrival time, using calculus or a + b ≥2 √ ab for positive a,b. (c) Find the launch angle and explain why the minimum is unique in positive T.
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Question 7 - Solution Minimize launch speed by choosing the flight time x y target (a) Solve the endpoint constraints for the launch components. v0x = 12/T, v0y = 5/T + 5T, v2 0 = 169/T 2 + 50 + 25T 2 (SI numerical T) v0x = 12 m/T and v0y = 5 m/T + (5 m/s2)T. With τ = T/(1 s), v2 0 = [169/τ 2 + 50 + 25τ 2] m2/s2. (b) Balance the two positive variable terms. 169 T 2 + 25T 2 ≥2 √ 169(25) = 130 ⇒ T = √ 13/5 s, v0,min = 6 √ 5 m/s 169/τ 2 + 25τ 2 ≥2 √ 169 · 25 = 130. Equality requires τ 2 = 13/5. Thus T = √ 13/5 ≈1.612 s and v0,min = √ 180 = 6 √ 5 ≈13.416 m/s. (c) Recover the optimum direction. tan θ = 5 + 5T 2 12 = 3 2 ⇒θ = 56.310◦, 169/T 2 = 25T 2 fixes T > 0 tan θ = v0y/v0x = (5 + 5τ 2)/12 = 18/12 = 3/2, so θ ≈56.310◦. The equality condition fixes one positive T; at either T approaching zero or infinity the required speed diverges. The minimum therefore selects a unique time and launch vector in this model.

Question 7

Minimize launch speed by choosing the flight time

A point target is at (12,5)(12,5) m relative to launch. You may choose any positive arrival time T and launch direction. Neglect air resistance and use uniform g=10m/s2g=10\ \mathrm{m/s^2} downward. Unless stated otherwise, x is horizontal and y upward. For this task minimize the initial speed; there are no obstacles.

Diagram shown in the original SVG worksheet.

  1. Express the required launch velocity components and squared speed as functions of T.

  2. Find the minimum speed and the corresponding arrival time, using calculus or a+b≥2aba+b\geq2\sqrt{ab} for positive a,b.

  3. Find the launch angle and explain why the minimum is unique in positive T.

Question 7 - Solution

Minimize launch speed by choosing the flight time

Diagram shown in the original SVG worksheet.

(a) Solve the endpoint constraints for the launch components.

v0x=12/T,v0y=5/T+5T,v02=169/T2+50+25T2(SI numerical T)v_{0x}=12/T,\quad v_{0y}=5/T+5T,\quad v_0^2=169/T^2+50+25T^2\quad\text{(SI numerical }T) v0x=12m/Tv_{0x}=12\ \mathrm m/T and v0y=5m/T+(5m/s2)Tv_{0y}=5\ \mathrm m/T+(5\ \mathrm{m/s^2})T. With τ=T/(1s)\tau=T/(1\ \mathrm s), v02=[169/τ2+50+25τ2]v_0^2=[169/\tau^2+50+25\tau^2] m2^2/s2^2.

(b) Balance the two positive variable terms.

169T2+25T2≥2169(25)=130⇒T=13/5s,v0,min=65m/s\frac{169}{T^2}+25T^2\ge2\sqrt{169(25)}=130\ \Rightarrow\ \boxed{T=\sqrt{13/5}\,\mathrm s,\quad v_{0,\min}=6\sqrt5\,\mathrm{m/s}} 169/τ2+25τ2≥2169⋅25=130169/\tau^2+25\tau^2\geq2\sqrt{169\cdot25}=130. Equality requires τ2=13/5\tau^2=13/5. Thus T=13/5≈1.612T=\sqrt{13/5}\approx1.612 s and v0,min=180=65≈13.416v_{0,\min}=\sqrt{180}=6\sqrt5\approx13.416 m/s.

(c) Recover the optimum direction.

tan⁡θ=5+5T212=32⇒θ=56.310∘,169/T2=25T2 fixes T>0\tan\theta=\frac{5+5T^2}{12}=\frac32\ \Rightarrow\ \theta=56.310^\circ,\quad169/T^2=25T^2\text{ fixes }T>0 tan⁡θ=v0y/v0x=(5+5τ2)/12=18/12=3/2\tan\theta=v_{0y}/v_{0x}=(5+5\tau^2)/12=18/12=3/2, so θ≈56.310∘\theta\approx56.310^\circ. The equality condition fixes one positive T; at either T approaching zero or infinity the required speed diverges. The minimum therefore selects a unique time and launch vector in this model.