The co-ordinates \((x, y, z)\) of a particle with respect to a uniformly rotating frame may be related to those with respect to a fixed inertial frame, \(\left(x^{*}, y^{*}, z^{*}\right)\), by the transformation $$ \left[\begin{array}{l} x \\ y \\ z \end{array}\right]=\left[\begin{array}{ccc} \cos \omega t & \sin \omega t & 0 \\ -\sin \omega t & \cos \omega t & 0 \\ 0 & 0 & 1 \end{array}\right]\left[\begin{array}{c} x^{*} \\ y^{*} \\ z^{*} \end{array}\right] $$ (Here, we use matrix notation: this stands for three separate equations, \(x=\cos \omega t \cdot x^{*}+\sin \omega t \cdot y^{*}\) etc.) Write down the inverse relation giving \(\left(x^{*}, y^{*}, z^{*}\right)\) in terms of \((x, y, z)\). By differentiating with respect to \(t\), rederive the relation (5.15) between \(\mathrm{d}^{2} \boldsymbol{r} / \mathrm{d} t^{2}\) and \(\ddot{\boldsymbol{r}}\). [Hint: Note that \(\ddot{\boldsymbol{r}}=(\ddot{x}, \ddot{y}, \ddot{z})\), while \(\mathrm{d}^{2} \boldsymbol{r} / \mathrm{d} t^{2}\) is the vector obtained by applying the above transformation \(\left.\operatorname{to}\left(\ddot{x}^{*}, \ddot{y}^{*}, \ddot{z}^{*}\right) .\right]\)

Short Answer

Expert verified
Question: Find the inverse relation for the given transformation matrix and rederive the relation between \(\frac{d^2 \textbf{r}}{dt^2}\) and \(\ddot{\textbf{r}}\). Answer: The inverse relation can be found by taking the transpose of the given orthogonal matrix: $$ \left[\begin{array}{c} x^* \\ y^* \\ z^* \end{array}\right]=\left[\begin{array}{ccc} \cos \omega t & -\sin \omega t & 0 \\ \sin \omega t & \cos \omega t & 0 \\ 0 & 0 & 1 \end{array}\right]\left[\begin{array}{c} x \\ y \\ z \end{array}\right] $$ After differentiating the matrix elements and applying the transformation, the rederived relation between \(\frac{d^2 \textbf{r}}{dt^2}\) and \(\ddot{\textbf{r}}\) is: $$ \frac{d^2 \textbf{r}}{dt^2} = \left[\begin{array}{ccc} \cos \omega t & -\sin \omega t & 0 \\ \sin \omega t & \cos \omega t & 0 \\ 0 & 0 & 1 \end{array}\right] \ddot{\textbf{r}} $$

Step by step solution

01

Find the Inverse Relation

To find the inverse relation, we need to find the inverse of the transformation matrix. The given transformation matrix is an orthogonal matrix, so its inverse is equal to its transpose. Therefore, the inverse relation can be obtained by transposing the given matrix: $$ \left[\begin{array}{c} x^* \\ y^* \\ z^* \end{array}\right]=\left[\begin{array}{ccc} \cos \omega t & -\sin \omega t & 0 \\ \sin \omega t & \cos \omega t & 0 \\ 0 & 0 & 1 \end{array}\right]\left[\begin{array}{c} x \\ y \\ z \end{array}\right] $$
02

Differentiate the Inverse Relation

Now, we differentiate the inverse relation with respect to time \(t\): $$ \frac{d}{dt}\left[\begin{array}{c} x^* \\ y^* \\ z^* \end{array}\right]=\frac{d}{dt}\left[\begin{array}{ccc} \cos \omega t & -\sin \omega t & 0 \\ \sin \omega t & \cos \omega t & 0 \\ 0 & 0 & 1 \end{array}\right]\left[\begin{array}{c} x \\ y \\ z \end{array}\right] + \left[\begin{array}{ccc} \cos \omega t & -\sin \omega t & 0 \\ \sin \omega t & \cos \omega t & 0 \\ 0 & 0 & 1 \end{array}\right]\frac{d}{dt}\left[\begin{array}{c} x \\ y \\ z \end{array}\right] $$
03

Differentiate the Matrix Elements

To find \(\frac{\text{d}^2 \textbf{r}}{\text{d}t^2}\) we need to differentiate both the elements of the inverse matrix and the coordinate vector \((x, y, z)\): $$ \frac{d^2}{dt^2}\left[\begin{array}{c} x^* \\ y^* \\ z^* \end{array}\right]=\frac{d^2}{dt^2}\left[\begin{array}{ccc} \cos \omega t & -\sin \omega t & 0 \\ \sin \omega t & \cos \omega t & 0 \\ 0 & 0 & 1 \end{array}\right]\left[\begin{array}{c} x \\ y \\ z \end{array}\right] + 2\frac{d}{dt}\left[\begin{array}{ccc} \cos \omega t & -\sin \omega t & 0 \\ \sin \omega t & \cos \omega t & 0 \\ 0 & 0 & 1 \end{array}\right]\frac{d}{dt}\left[\begin{array}{c} x \\ y \\ z \end{array}\right] + \left[\begin{array}{ccc} \cos \omega t & -\sin \omega t & 0 \\ \sin \omega t & \cos \omega t & 0 \\ 0 & 0 & 1 \end{array}\right]\frac{d^2}{dt^2}\left[\begin{array}{c} x \\ y \\ z \end{array}\right] $$
04

Derive the Relation between \(\frac{\text{d}^2 \textbf{r}}{\text{d}t^2}\) and \(\ddot{\textbf{r}}\)

After differentiating the matrix elements, we need to apply the transformation to \((\ddot{x^*}, \ddot{y^*}, \ddot{z^*})\) and rederive the relation: $$ \frac{d^2 \textbf{r}}{dt^2} = \left[\begin{array}{ccc} \cos \omega t & -\sin \omega t & 0 \\ \sin \omega t & \cos \omega t & 0 \\ 0 & 0 & 1 \end{array}\right]\left[\begin{array}{c} \ddot{x^*} \\ \ddot{y^*} \\ \ddot{z^*} \end{array}\right] $$ Now, we apply the transformation to \((\ddot{x^*}, \ddot{y^*}, \ddot{z^*})\) and substitute \(\ddot{\textbf{r}} = (\ddot{x}, \ddot{y}, \ddot{z})\): $$ \frac{d^2 \textbf{r}}{dt^2} = \left[\begin{array}{ccc} \cos \omega t & -\sin \omega t & 0 \\ \sin \omega t & \cos \omega t & 0 \\ 0 & 0 & 1 \end{array}\right] \ddot{\textbf{r}} $$ This is the rederived relation between \(\frac{d^2 \textbf{r}}{dt^2}\) and \(\ddot{\textbf{r}}\), as we were asked to find.

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Most popular questions from this chapter

Water in a rotating container of radius \(50 \mathrm{~mm}\) is \(30 \mathrm{~mm}\) lower in the centre than at the edge. Find the angular velocity of the container.

Another way of deriving the equation of motion (5.16) is to use Lagrange's equations. Express the kinetic energy \(\frac{1}{2} m(\mathrm{~d} \boldsymbol{r} / \mathrm{d} t)^{2}\) in terms of \((x, y, z)\), and show that Lagrange's equations (3.44) reproduce (5.16) for the case where the force is conservative.

A projectile is launched due north from a point in colatitude \(\theta\) at an angle \(\pi / 4\) to the horizontal, and aimed at a target whose distance is \(y\) (small compared to Earth's radius \(R\) ). Show that if no allowance is made for the effects of the Coriolis force, the projectile will miss its target by a distance \(x=\omega\left(\frac{2 y^{3}}{g}\right)^{1 / 2}\left(\cos \theta-\frac{1}{3} \sin \theta\right)\) Evaluate this distance if \(\theta=45^{\circ}\) and \(y=40 \mathrm{~km}\). Why is it that the deviation is to the east near the north pole, but to the west both on the equator and near the south pole? (Neglect atmospheric resistance.)

Find the velocity relative to an inertial frame (in which the centre of the Earth is at rest) of a point on the Earth's equator. An aircraft is flying above the equator at \(1000 \mathrm{~km} \mathrm{~h}^{-1}\). Assuming that it flies straight and level (i.e., at a constant altitude above the surface) what is its velocity relative to the inertial frame (a) if it flies north, (b) if it flies west, and (c) if it flies east?

An orbiting space station may be made to rotate to provide an artificial gravity. Given that the radius is \(25 \mathrm{~m}\), find the rotation period required to produce an apparent gravity equal to \(0.7 g\). A man whose normal weight is \(75 \mathrm{~kg}\) weight runs around the station in one direction and then the other (i.e., on a circle on the inside of the cylindrical wall) at \(5 \mathrm{~ms}^{-1}\). Find his apparent weight in each case. What effects will he experience if he climbs a ladder to a higher level ( i.e., closer to the axis), climbing at \(1 \mathrm{~ms}^{-1} ?\)

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