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.

Short Answer

Expert verified
To summarize, we derived the equation of motion using Lagrange's equations by performing the following steps: 1. We expressed the kinetic energy in terms of (x, y, z): \(T = \frac{1}{2}m\left(\left(\frac{\mathrm{d}x}{\mathrm{d}t}\right)^2 + \left(\frac{\mathrm{d}y}{\mathrm{d}t}\right)^2 + \left(\frac{\mathrm{d}z}{\mathrm{d}t}\right)^2\right)\) 2. We wrote out Lagrange's equations for each coordinate (x, y, z): - \(m\ddot{x} = Q_x\) - \(m\ddot{y} = Q_y\) - \(m\ddot{z} = Q_z\) 3. We showed that these equations reproduce equation (5.16) when the force is conservative, resulting in the following equations: - \(m\ddot{x} = -\frac{\partial U}{\partial x}\) - \(m\ddot{y} = -\frac{\partial U}{\partial y}\) - \(m\ddot{z} = -\frac{\partial U}{\partial z}\) Hence, Lagrange's equations can be used to derive the equation of motion for conservative forces.

Step by step solution

01

Express the kinetic energy in terms of (x, y, z)

First, we'll express the given kinetic energy \(\frac{1}{2}m(\frac{\mathrm{d}\boldsymbol{r}}{\mathrm{d}t})^2\) in terms of \((x, y, z)\). We know that \(\boldsymbol{r} = x\boldsymbol{\hat{i}} + y\boldsymbol{\hat{j}} + z\boldsymbol{\hat{k}}\). Then, we can differentiate \(\boldsymbol{r}\) with respect to time and get the velocity vector \(\boldsymbol{v} = \frac{\mathrm{d}\boldsymbol{r}}{\mathrm{d}t} = \frac{\mathrm{d}x}{\mathrm{d}t}\boldsymbol{\hat{i}} + \frac{\mathrm{d}y}{\mathrm{d}t}\boldsymbol{\hat{j}} + \frac{\mathrm{d}z}{\mathrm{d}t}\boldsymbol{\hat{k}}\). Now, we can find the square of the velocity vector's magnitude: \((\boldsymbol{v})^2 = \left(\frac{\mathrm{d}x}{\mathrm{d}t}\right)^2 + \left(\frac{\mathrm{d}y}{\mathrm{d}t}\right)^2 + \left(\frac{\mathrm{d}z}{\mathrm{d}t}\right)^2\) Then, the kinetic energy in terms of \((x, y, z)\) is given by \(T = \frac{1}{2}m\left(\left(\frac{\mathrm{d}x}{\mathrm{d}t}\right)^2 + \left(\frac{\mathrm{d}y}{\mathrm{d}t}\right)^2 + \left(\frac{\mathrm{d}z}{\mathrm{d}t}\right)^2\right)\)
02

Write out Lagrange's equations

Lagrange's equations are given by \(\frac{\mathrm{d}}{\mathrm{d}t}\left(\frac{\partial T}{\partial \dot{q}_i}\right) - \frac{\partial T}{\partial q_i} = Q_i\), where \(q_i\) represents the generalized coordinates (in this case, \(x, y, z\)) and \(Q_i\) are the generalized forces. So, we need to calculate \(\frac{\partial T}{\partial \dot{x}}, \frac{\partial T}{\partial \dot{y}}, \frac{\partial T}{\partial \dot{z}}, \frac{\partial T}{\partial x}, \frac{\partial T}{\partial y}, \frac{\partial T}{\partial z}\). Since \(T\) is dependent only on the velocities, we have \(\frac{\partial T}{\partial x} = \frac{\partial T}{\partial y} = \frac{\partial T}{\partial z} = 0\). And we can determine the partial derivatives with respect to the velocities as \(\frac{\partial T}{\partial \dot{x}} = m\dot{x}, \frac{\partial T}{\partial \dot{y}} = m\dot{y}, \frac{\partial T}{\partial \dot{z}} = m\dot{z}\). Now, let's write Lagrange's equations for each coordinate: 1. For \(x\): \(\frac{\mathrm{d}}{\mathrm{d}t}\left(\frac{\partial T}{\partial \dot{x}}\right) - \frac{\partial T}{\partial x} = m\ddot{x} = Q_x\) 2. For \(y\): \(\frac{\mathrm{d}}{\mathrm{d}t}\left(\frac{\partial T}{\partial \dot{y}}\right) - \frac{\partial T}{\partial y} = m\ddot{y} = Q_y\) 3. For \(z\): \(\frac{\mathrm{d}}{\mathrm{d}t}\left(\frac{\partial T}{\partial \dot{z}}\right) - \frac{\partial T}{\partial z} = m\ddot{z} = Q_z\)
03

Show that the equations reproduce (5.16) for conservative forces

When the force is conservative, we can express the force as the negative gradient of a potential energy function \(U(x, y, z)\), i.e., \(\boldsymbol{F} = -\boldsymbol{\nabla}U\). Thus for each component of the force, we have \(Q_x = -\frac{\partial U}{\partial x}\), \(Q_y = -\frac{\partial U}{\partial y}\), and \(Q_z = -\frac{\partial U}{\partial z}\). Let's substitute these into the Lagrange's equations from Step 2: 1. \(m\ddot{x} = -\frac{\partial U}{\partial x}\) 2. \(m\ddot{y} = -\frac{\partial U}{\partial y}\) 3. \(m\ddot{z} = -\frac{\partial U}{\partial z}\) These equations are equivalent to equation (5.16) for conservative forces. Therefore, we have shown that Lagrange's equations can be used to derive the equation of motion.

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with Vaia!

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

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 aircraft is flying at \(800 \mathrm{~km} \mathrm{~h}^{-1}\) in latitude \(55^{\circ} \mathrm{N}\). Find the angle through which it must tilt its wings to compensate for the horizontal component of the Coriolis force.

Find the equation of motion for a particle in a uniformly accelerated frame, with acceleration \(\boldsymbol{a} .\) Show that for a particle moving in a uniform gravitational field, and subject to other forces, the gravitational field may be eliminated by a suitable choice of \(\boldsymbol{a}\).

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 \(\left.\operatorname{to}\left(\ddot{x}^{*}, \ddot{y}^{*}, \ddot{z}^{*}\right) .\right]\)

The orbit of an electron (charge \(-e)\) around a nucleus (charge \(Z e\) ) is a circle of radius \(a\) in a plane perpendicular to a uniform magnetic field \(\boldsymbol{B}\). By writing the equation of motion in a frame rotating with the electron, show that the angular velocity \(\omega\) is given by one of the roots of the equation \(m \omega^{2}-e B \omega-Z e^{2} / 4 \pi \epsilon_{0} a^{3}=0\) Verify that for small values of \(B\), this agrees with \(\S 5.5\). Evaluate the two roots if \(B=10^{5} \mathrm{~T}, Z=1\) and \(a=5.3 \times 10^{-11} \mathrm{~m}\). (Note, however, that in reality \(a\) would be changed by the field.)

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.

Sign-up for free