A spacecraft travels in a plane using a guidance system that reports its velocity in…

MATHEMATICS · Multi-part · AP · AP Precalculus · Functions with Parameters, Vectors, and Matrices · Functions with Parameters, Vectors, and Matrices

Problem

A spacecraft travels in a plane using a guidance system that reports its velocity in polar coordinates relative to a fixed origin. For 0≤t≤10\le t\le1 hour, the radial and angular velocity components are drdt=5t(kilometers per hour),dθdt=t2(radians per hour),\frac{dr}{dt}=5t\quad\text{(kilometers per hour)},\qquad\frac{d\theta}{dt}=t^{2}\quad\text{(radians per hour)}, where r(t)r(t) is the distance from the origin in kilometers and θ(t)\theta(t) is the polar angle measured from the positive xx–axis. At t=0t=0, the spacecraft is located at polar coordinates (r,θ)=(2,0)(r,\theta)=(2,0). (a) Determine r(t)r(t) for 0≤t≤10\le t\le1 hour. (b) Determine θ(t)\theta(t) for 0≤t≤10\le t\le1 hour. (c) Express the spacecraft’s position at t=1t=1 hour in Cartesian coordinates ⟨x,y⟩\langle x,y\rangle (kilometers). (d) Compute the spacecraft’s speed at t=1t=1 hour and interpret this value in the context of the problem.

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