Polar coordinates and kinematics

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SUMMARY

The discussion focuses on deriving polar equations for a rocket's motion under acceleration in polar coordinates. The user seeks assistance in formulating the position, velocity, and acceleration equations, specifically for the radial distance r(t) and the angular component. Key equations mentioned include r(t)=r\vec{e_r}, v(t)=\dot r\vec{e_r}+r\dot \theta\vec{e_{\theta}}, and a(t)=(\ddot r-r\dot \theta^2)\vec{e_r}+(r\ddot \theta+2 \dot r \dot \theta)\vec{e_{\theta}}. The user expresses uncertainty about incorporating acceleration into their calculations and seeks clarification on using trigonometric functions for this purpose.

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  • Understanding of polar coordinates and their applications in kinematics
  • Familiarity with vector calculus and motion equations
  • Knowledge of trigonometric functions and their properties
  • Basic principles of acceleration and its components in polar coordinates
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  • Study the derivation of polar coordinate equations in kinematics
  • Learn how to apply trigonometric identities in polar motion problems
  • Explore the relationship between radial and angular acceleration in polar coordinates
  • Review examples of motion in polar coordinates, focusing on acceleration components
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Telemachus
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Homework Statement


I've got some trouble and doubts with polar coordinates. I have this exercise, with a rocket going upwards, with a given acceleration. So I need to find the polar equation for the given situation for the position, the velocity and the acceleration. How should I proceed? I mean, I know I must find an equation that describes the path for r(t) in the polar form, but I'm not sure on how the acceleration fit on this.

attachment.php?attachmentid=28831&stc=1&d=1286321434.png


The distance between the origin and the rocket "D" is given by the problem data.

Homework Equations


[tex]r(t)=r\vec{e_r}[/tex]
[tex]v(t)=\dot r\vec{e_r}+r\dot \theta\vec{e_{\theta}}[/tex]
[tex]a(t)=(\ddot r-r\dot \theta^2)\vec{e_r}+(r\ddot \theta+2 \dot r \dot \theta)\vec{e_{\theta}}[/tex]

I think that [tex]r(t)[/tex] could be: [tex]r(t)=\sec \theta \vec{e_r}[/tex], but then I don't know how to work with the acceleration on the radial direction, or over the angle direction neither. Should I use trigonometry for this?
 

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I've tried this way, but it doesn't looks fine really

[tex]a=k[/tex], [tex]s=kt[/tex] [tex]x=\displaystyle\frac{k}{2}t^2[/tex]

Then the radial speed:
[tex]\dot r=s \cos \theta=kt \cos \theta[/tex]

And the angular speed:
[tex]\dot \theta=s \sin \theta=kt \sin \theta[/tex]

I think that the equation for r(t) should be [tex]\vec{r(t)}=\sec \theta \hat{e_r}[/tex]. But I don't know how to work with it.

[tex]\dot r=v(t)=\dot r\vec{e_r}+r\dot \theta\vec{e_{\theta}}[/tex]
[tex]\dot r=\sec r \tan r\hat{e_r}+\sec r \dot \theta \hat{e_{\theta}}[/tex]

I don't know how to determine the radial speed and the angular speed, considering the acceleration, and I think what I've done doesn't make any sense.

Any help please?
Bye there.
 

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