How to solve this problem in sinusoidal motion? (Satellite orbiting the Earth)

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Homework Help Overview

The discussion revolves around a problem related to sinusoidal motion, specifically focusing on a satellite orbiting the Earth. Participants are examining calculations involving angular frequency, frequency, and the implications of these values in the context of orbital mechanics.

Discussion Character

  • Exploratory, Assumption checking, Mathematical reasoning

Approaches and Questions Raised

  • Participants discuss the calculation of angular frequency and frequency, noting discrepancies in the original poster's results. Questions are raised about the validity of the formulas used and the expected values for acceleration and velocity in the context of orbital motion.

Discussion Status

There is an ongoing exploration of the calculations presented, with some participants suggesting comparisons to known values for geosynchronous orbits. Guidance is offered regarding unit checks and the implications of the results, but no consensus has been reached on the correctness of the original poster's approach.

Contextual Notes

Participants are considering the altitude of the satellite and its relation to geosynchronous orbit, as well as the expected values for acceleration at different radii. There is an acknowledgment of potential errors in the original calculations, but no specific resolutions have been proposed.

Safinaz
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Homework Statement
A satellite orbits the Earth at a speed of 3100 m/s in an orbit that passes through the north and south points and has a radius of ##4.2 \times10^7## m. Consider a point moving in a straight line along the north-south axis of the Earth and passing through its center such that its speed is always equal to the component of the satellite's velocity in the north-south direction. Find a) the frequency of the point's motion, b) the acceleration of the point at the two end points of the motion, and c) its maximum speed.
Relevant Equations
The angular frequency : ## \omega= \frac{v}{x}##

The frequency ## f= 2 \pi \omega ##

For a SHM: ## a = - \omega^2 x##

The maximum velocity: ## v = - v_{max} sin ( 2 \pi f t ) ##
I tried to solve by calculating:

## \omega = \frac{v}{x} = 3100/ (4.2 \times10^7) ##,

Which makes the frequency so small:
## f = 2 \pi \times 3100/ (4.2 \times10^7) \sim 10^{-5} ~ s^{-1} ##

And also the acceleration and velocity. So I think there is a mistake in my solution.

Any help to solve this problem accurately is appreciated.
 
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Safinaz said:
Which makes the frequency so small:
## f = 2 \pi \times 3100/ (4.2 \times10^7) \sim 10^{-5} ~ s^{-1} ##
You could look up the altitude for geosynchronous orbit and compare that to ##4.2 \times 10^7## meters.

What is the frequency for geosynchronous orbit?
 
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Safinaz said:
The frequency ## f= 2 \pi \omega ##
Check the units: radians/cycle x radians/second =?
Safinaz said:
Which makes the frequency so small:
## f = 2 \pi \times 3100/ (4.2 \times10^7) \sim 10^{-5} ~ s^{-1} ##
What does that make the orbital period to be? Is that unreasonable?
 
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haruspex said:
Check the units: radians/cycle x radians/second =?
While OP has written down the wrong formula, their numerical result corresponds to the correct one.
 
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Safinaz said:
And also the acceleration and velocity. So I think there is a mistake in my solution.
Here is another reality check for your solution. Why do you think your acceleration is small? What do you expect it to be at a radius of 42000 km given that it is about 10 m/s^2 at the Earth radius 6700 km?
 

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