Elliptical motion in polar coordinates

  • #1
lorenz0
148
28
Homework Statement
Given that ##x(t)=a\cos(\Omega t)## and ##y(t)=b\sin(\Omega t)##, identify the trajectory and then find the position and velocity vectors in polar coordinates.
Relevant Equations
##\vec{r}=r\hat{r}=\sqrt{x^2+y^2}\hat{r}##, ##\theta=\arctan\left(\frac{y}{x}\right)##, ##\vec{v}=\frac{dr}{dt}\hat{r}+r\frac{d\hat{r}}{dt}=\frac{dr}{dt}\hat{r}+r\frac{d\theta}{dt}\hat{\theta}##
I think I have completed the exercise but since I have seldom used polar coordinates I would be grateful if someone would check out my work and tell me if I have done everything correctly. Thanks.
My solution follows.

Since ##\left(\frac{x}{a}\right)^2+\left(\frac{y}{b}\right)^2=1## it follows that the trajectory is an ellipse centered at the origin with axes ##a## and ##b.## Now, ##\vec{r}=r\hat{r}=\sqrt{x^2+y^2}\hat{r}=\sqrt{a^2\cos^2(\Omega t)+b^2\sin^2(\Omega t)}\hat{r}## and
##\theta=\arctan\left(\frac{y}{x}\right)=\arctan\left(\frac{b}{a}\tan(\Omega t)\right)## so, since ##\frac{dr}{dt}=\frac{-2a^2\cos(\Omega t)\sin(\Omega t)\Omega+2b^2\cos(\Omega t)\sin(\Omega t)\Omega}{2\sqrt{a^2\cos^2(\Omega t)+b^2\sin(\Omega t)}}=\frac{(b^2-a^2)\Omega\sin(2\Omega t)}{2r}## and ##\frac{d\theta}{dt}=\frac{1}{1+\left(\frac{b}{a}\tan(\Omega t)\right)^2}\cdot\frac{b}{a}\cdot \frac{1}{\cos^2(\Omega t)}\cdot\Omega=\frac{a^2\cos^2(\Omega t)}{a^2\cos^2(\Omega t)+b^2\sin^2(\Omega t)}\cdot\frac{b}{a}\cdot\frac{1}{\cos^2(\Omega t)}\cdot\Omega=\frac{ab\Omega}{r^2}## we have that
\begin{align*}
\vec{v}&=\frac{dr}{dt}\hat{r}+r\frac{d\hat{r}}{dt}=\frac{dr}{dt}\hat{r}+r\frac{d\theta}{dt}\hat{\theta}\\ &=\frac{(b^2-a^2)\Omega\sin(2\Omega t)}{2r}\hat{r}+r\frac{ab\Omega}{r^2}\hat{\theta}\\
&=\frac{(b^2-a^2)\Omega\sin(2\Omega t)}{2r}\hat{r}+\frac{ab\Omega}{r}\hat{\theta}
\end{align*}
 
Last edited:
Physics news on Phys.org
  • #2
Why do you have the squared tangent in the ##\theta (t)## calculation? (OP was edited).
 
  • #3
dextercioby said:
Why do you have the squared tangent in the ##\theta (t)## calculation?
Typo. Fixed, thanks.
 
  • #4
Please fix the whole calculation. There's no 2 anymore, since there's no square in the argument of ##\arctan ## (OP was again edited).
 
Last edited:
  • #5
dextercioby said:
Please fix the whole calculation. There's no 2 anymore, since there's no square in the argument of ##\arctan ##.
Done.
 
  • #7
dextercioby said:
Much better.
Thanks!
 
  • #8
Sorry, there's an error in the ##\frac{dr}{dt}## calculation. The derivative of ##\cos## carries a minus.
 
  • Like
Likes lorenz0
  • #9
dextercioby said:
Sorry, there's an error in the ##\frac{dr}{dt}## calculation. The derivative of ##\cos## carries a minus.
Corrected. Thanks again.
 
  • #10
Sorry, last check also in ##\frac{dr}{dt}## calculation. The 2 in the denominator stays there, if you use the 2 in the numerator to obtain the ##\sin## of double angle, right?
 
  • Like
Likes lorenz0
  • #11
dextercioby said:
Sorry, last check also in ##\frac{dr}{dt}## calculation. The 2 in the denominator stays there, if you use the 2 in the numerator to obtain the ##\sin## of double angle, right?
You are right.
 

FAQ: Elliptical motion in polar coordinates

What is elliptical motion in polar coordinates?

Elliptical motion in polar coordinates describes the path of an object moving along an ellipse, where the position of the object is given in terms of the radius (distance from the focus) and the angle (measured from a reference direction). This is useful in orbital mechanics to describe planetary orbits.

How do you represent an ellipse in polar coordinates?

An ellipse in polar coordinates can be represented by the equation \( r(\theta) = \frac{a(1 - e^2)}{1 + e \cos(\theta)} \), where \( r \) is the radius, \( \theta \) is the angle, \( a \) is the semi-major axis, and \( e \) is the eccentricity of the ellipse.

What is the significance of the eccentricity in elliptical motion?

The eccentricity \( e \) of an ellipse determines the shape of the ellipse. If \( e = 0 \), the ellipse is a circle. If \( 0 < e < 1 \), the ellipse is elongated. Higher values of \( e \) indicate a more elongated ellipse, while values close to 0 indicate an almost circular shape.

How do you derive the equation of motion for an object in an elliptical orbit?

The equation of motion for an object in an elliptical orbit can be derived using Newton's laws of motion and gravitation. By solving the differential equations that result from these laws, one can obtain the orbit equation in polar coordinates, which is \( r(\theta) = \frac{p}{1 + e \cos(\theta)} \), where \( p \) is the semi-latus rectum of the ellipse.

What are the applications of elliptical motion in polar coordinates?

Elliptical motion in polar coordinates is widely used in astrophysics and orbital mechanics to predict and describe the orbits of planets, moons, and artificial satellites. It is also used in engineering fields related to space travel and satellite deployment.

Back
Top