- Calculus, Volume 1: One Variable Calculus, with an Introduction to Linear Algebra
- Tom M. Apostol
- Second Edition
- 1967
- 978-1-119-49673-1
14.19 Exercises
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A missile is designed to move directly toward its target. Due to mechanical failure, its direction in actual flight makes a fixed angle $\alpha \neq 0$ with the line from the missile to the target. Find the path if it is fired at a fixed target. Discuss how the path varies with $\alpha.$ Does the missile ever reach the target? (Assume the motion takes place in a plane.)
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If the direction of the missile makes a fixed angle $\alpha \neq 0$ with the target, then it implies that $\alpha$ is the angle between $\mathbf{v}(t)$ and $-\mathbf{r}(t).$ Use this along with the result of Exercise 14 to yield a separable differential equation in $r$ and $\theta.$
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Suppose the target is at the origin, and the missile is fired from starting position $(r_0, 0).$ Then, if the direction of the missile makes a fixed angle $\alpha \neq 0$ with the target, this implies that $\alpha$ is in fact the angle between $\mathbf{v}(t)$ and $-\mathbf{r}(t).$ Recall from Exercise 14 that if $\alpha$ is the angle between the position vector and velocity vector, where the curve is expressed in polar coordinates, then $r = v\sin\alpha$ and $\frac{dr}{d\theta} = -v\cos\alpha$ where $r = \|\mathbf{r}\|$ and $v = \|\mathbf{v}\|.$ This gives us the following separable differential equation:
\begin{align*}
\\
\frac{1}{r}\frac{dr}{d\theta} &= -\cot\alpha
\end{align*}
Separating terms by $r$ and $\theta$ gives us:
\begin{align*}
\\
\frac{dr}{r} &= -\cot\alpha\,d\theta
\end{align*}
Integrating from $x = 0$ to $x = \theta,$ applying the second fundamental theorem, we get:
\begin{align*}
\\
\int_{r_0}^{r}\frac{du}{u} &= -\cot\alpha\int_{0}^{\theta}dx
\\
\\
\log\,r - \log\,r_0 &= -\theta\cot\alpha
\end{align*}
Rearranging terms and exponentiating both sides, we get
\begin{align*}
\
r &= r_0e^{-\theta\cot\alpha}
\end{align*}
The path of the missile can be described in three possible cases dependent on $\alpha:$
1. If $0 < \alpha < \frac{\pi}{2},$ then $-\cot\alpha < 0$ and the path of the missile is a spiral whose radius approaches $0$ as $\theta$ grows indefinitely.
2. If $\alpha = \frac{\pi}{2},$ then $-\cot\alpha = 0$ and the path of the missile is a circle centered about the target with radius $r_0.$
3. If $\frac{\pi}{2} < \alpha < \pi,$ then $-\cot\alpha > 0$ and the path of the missile is a spiral whose radius grows without bound as $\theta$ grows indefinitely. $\blacksquare$