41.1: The Simple Plane Pendulum
- Page ID
- 92287
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\(\newcommand{\avec}{\mathbf a}\) \(\newcommand{\bvec}{\mathbf b}\) \(\newcommand{\cvec}{\mathbf c}\) \(\newcommand{\dvec}{\mathbf d}\) \(\newcommand{\dtil}{\widetilde{\mathbf d}}\) \(\newcommand{\evec}{\mathbf e}\) \(\newcommand{\fvec}{\mathbf f}\) \(\newcommand{\nvec}{\mathbf n}\) \(\newcommand{\pvec}{\mathbf p}\) \(\newcommand{\qvec}{\mathbf q}\) \(\newcommand{\svec}{\mathbf s}\) \(\newcommand{\tvec}{\mathbf t}\) \(\newcommand{\uvec}{\mathbf u}\) \(\newcommand{\vvec}{\mathbf v}\) \(\newcommand{\wvec}{\mathbf w}\) \(\newcommand{\xvec}{\mathbf x}\) \(\newcommand{\yvec}{\mathbf y}\) \(\newcommand{\zvec}{\mathbf z}\) \(\newcommand{\rvec}{\mathbf r}\) \(\newcommand{\mvec}{\mathbf m}\) \(\newcommand{\zerovec}{\mathbf 0}\) \(\newcommand{\onevec}{\mathbf 1}\) \(\newcommand{\real}{\mathbb R}\) \(\newcommand{\twovec}[2]{\left[\begin{array}{r}#1 \\ #2 \end{array}\right]}\) \(\newcommand{\ctwovec}[2]{\left[\begin{array}{c}#1 \\ #2 \end{array}\right]}\) \(\newcommand{\threevec}[3]{\left[\begin{array}{r}#1 \\ #2 \\ #3 \end{array}\right]}\) \(\newcommand{\cthreevec}[3]{\left[\begin{array}{c}#1 \\ #2 \\ #3 \end{array}\right]}\) \(\newcommand{\fourvec}[4]{\left[\begin{array}{r}#1 \\ #2 \\ #3 \\ #4 \end{array}\right]}\) \(\newcommand{\cfourvec}[4]{\left[\begin{array}{c}#1 \\ #2 \\ #3 \\ #4 \end{array}\right]}\) \(\newcommand{\fivevec}[5]{\left[\begin{array}{r}#1 \\ #2 \\ #3 \\ #4 \\ #5 \\ \end{array}\right]}\) \(\newcommand{\cfivevec}[5]{\left[\begin{array}{c}#1 \\ #2 \\ #3 \\ #4 \\ #5 \\ \end{array}\right]}\) \(\newcommand{\mattwo}[4]{\left[\begin{array}{rr}#1 \amp #2 \\ #3 \amp #4 \\ \end{array}\right]}\) \(\newcommand{\laspan}[1]{\text{Span}\{#1\}}\) \(\newcommand{\bcal}{\cal B}\) \(\newcommand{\ccal}{\cal C}\) \(\newcommand{\scal}{\cal S}\) \(\newcommand{\wcal}{\cal W}\) \(\newcommand{\ecal}{\cal E}\) \(\newcommand{\coords}[2]{\left\{#1\right\}_{#2}}\) \(\newcommand{\gray}[1]{\color{gray}{#1}}\) \(\newcommand{\lgray}[1]{\color{lightgray}{#1}}\) \(\newcommand{\rank}{\operatorname{rank}}\) \(\newcommand{\row}{\text{Row}}\) \(\newcommand{\col}{\text{Col}}\) \(\renewcommand{\row}{\text{Row}}\) \(\newcommand{\nul}{\text{Nul}}\) \(\newcommand{\var}{\text{Var}}\) \(\newcommand{\corr}{\text{corr}}\) \(\newcommand{\len}[1]{\left|#1\right|}\) \(\newcommand{\bbar}{\overline{\bvec}}\) \(\newcommand{\bhat}{\widehat{\bvec}}\) \(\newcommand{\bperp}{\bvec^\perp}\) \(\newcommand{\xhat}{\widehat{\xvec}}\) \(\newcommand{\vhat}{\widehat{\vvec}}\) \(\newcommand{\uhat}{\widehat{\uvec}}\) \(\newcommand{\what}{\widehat{\wvec}}\) \(\newcommand{\Sighat}{\widehat{\Sigma}}\) \(\newcommand{\lt}{<}\) \(\newcommand{\gt}{>}\) \(\newcommand{\amp}{&}\) \(\definecolor{fillinmathshade}{gray}{0.9}\)A simple plane pendulum is a pendulum that consists of a point mass \(m\) at the end of a string of length \(L\) of negligible mass (Fig. \(\PageIndex{1}\)). The pendulum is displaced from vertical by an angle \(\theta_{0}\) and released; after that, it swings back and forth under the influence of gravity. The pendulum is constrained to swing back and forth in a plane.

When the pendulum makes an angle \(\theta\) from the vertical, the torque acting to move it back toward vertical
is \(-m g L \sin \theta\). Then by the rotational version of Newton's second law of motion,
\[\tau =I \alpha \]
\[-m g L \sin \theta =m L^{2} \frac{d^{2} \theta}{d t^{2}} \]
\[\frac{d^{2} \theta}{d t^{2}} =-\frac{g}{L} \sin \theta\]
This is a second-order differential equation that is fairly difficult to solve; the solution is shown in Appendix S. If we constrain the pendulum to small angles \(\theta\), then we can make the approximation
\[\sin \theta \approx \theta \quad(\theta \text { in radians }) .\]
Under this approximation, Eq. (38.3) becomes
\[\frac{d^{2} \theta}{d t^{2}}=-\frac{g}{L} \theta\]
This is a second-order differential equation that's fairly easy to solve; you'll learn how to solve differential equations like this in a course on differential equations. The solution turns out to be
\[\theta(t)=\theta_{0} \cos (\omega t+\delta)\]
where \(\theta_{0}\) is the (angular) amplitude of the motion (in radians), \(\omega=\sqrt{g / L}\) is the angular frequency of the motion (rad/s), and \(\delta\) is an arbitrary integration constant (seconds). The solution can be verified by direct substitution into Eq. (38.5).
The period \(T\) of the motion (the time required for one complete back-and-forth cycle) is given by
\[T=\frac{2 \pi}{\omega}\]
or
\[T=2 \pi \sqrt{\frac{L}{g}}\]
Remember that this is an approximation, and is valid only for small \(\theta\). The period of motion for a large period is given by an infinite series, and is shown in Appendix S.