I don't know yet how to integrate this function....

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SUMMARY

The discussion focuses on calculating the distance traveled by a point on Earth as it orbits the sun while also rotating. The user simplifies the Earth's orbit to a straight line for approximation and seeks to integrate a function that accounts for both the Earth's rotation and translation. Key equations provided include parametric equations for the trajectory: x(t) = Ra*cos(2*pi t/Ta) + Rb*cos(2*pi*t/Tb)*cos(latitude) and y(t) = Ra*sin(2*pi t/Ta) + Rb*sin(2*pi*t/Tb)*cos(latitude). The user ultimately resolves the integration challenge using a Taylor series approach.

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  • Understanding of parametric equations in physics
  • Familiarity with integration techniques, including numerical integration
  • Knowledge of Earth's orbital mechanics, including radius and period
  • Basic concepts of trigonometry and Taylor series
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Students and professionals in physics, particularly those interested in orbital mechanics, numerical methods, and integration techniques. This discussion is beneficial for anyone looking to understand the complexities of motion in a rotating and translating frame of reference.

pabilbado
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I was just wondering about the path an orbiting particle takes when it's center of circular motion also translates. So as to calculate the distance traveled I know I have to get a function that relates velocity with respect to time and integrate it, but I can't doit, I get stuck integrating. I have search the Internet across and nothing. Possibly I don't know what I am looking for. Here is the function:
df40425500452af6d860f2e1c2e4efdb.png

I can simplify it but it continues being difficult:
ba863ee3701d465bae822f56ed19c330.png
 
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Is this a homework problem?
 
Dr. Courtney said:
Is this a homework problem?
No, is not. Two days ago it was my father's birthday (he is a nerdy engineer so he will like this kind of present) so I am trying to calculate how much kilometers he has traveled around the sun. And as an approximation I have made the Earth's orbit a straight line, and this is the result of a point on Earth rotating and translating.
 
pabilbado said:
No, is not. Two days ago it was my father's birthday (he is a nerdy engineer so he will like this kind of present) so I am trying to calculate how much kilometers he has traveled around the sun. And as an approximation I have made the Earth's orbit a straight line, and this is the result of a point on Earth rotating and translating.
I don't know how you can make an orbit a straight line.

If you want to know how far your father has traveled in his lifetime, assume that Earth's orbit is a circle with a radius of 150 million kilometers. Every year, the Earth makes one orbit of the sun, by definition. The eccentricity of Earth's orbit is about 0.017, so a circle is a good approximation for all practical purposes here.
 
SteamKing said:
I don't know how you can make an orbit a straight line.

If you want to know how far your father has traveled in his lifetime, assume that Earth's orbit is a circle with a radius of 150 million kilometers. Every year, the Earth makes one orbit of the sun, by definition. The eccentricity of Earth's orbit is about 0.017, so a circle is a good approximation for all practical purposes here.

Yeah, that's the easy way. What I want is to take into account the rotation of earth, while is moving around the sun. Because a point in the surface of the Earth does not travel a circular path around the sun but rather a really "curly" trajectory. So as a first approximation I have flattened Earth's orbit so it is just traveling in a straight line and I need to take into consideration the that the point is also rotating. That wwhat the integral is for.
 
Why not write the parametric equations as:

x(t) = Ra*cos(2*pi t/Ta) + Rb*cos(2*pi*t/Tb)*cos(latitude)
y(t) = Ra*sin(2*pi t/Ta) + Rb*sin(2*pi*t/Tb)*cos(latitude)

Use the arc length integral, substitute in, and integrate numerically.

Ra, Ta = radius and period of Earth's orbit
Rb = Earth's radius, Tb = one day

Hopefully, you can treat the latitude as constant.
 
Dr. Courtney said:
Why not write the parametric equations as:

x(t) = Ra*cos(2*pi t/Ta) + Rb*cos(2*pi*t/Tb)*cos(latitude)
y(t) = Ra*sin(2*pi t/Ta) + Rb*sin(2*pi*t/Tb)*cos(latitude)

Use the arc length integral, substitute in, and integrate numerically.

Ra, Ta = radius and period of Earth's orbit
Rb = Earth's radius, Tb = one day

Hopefully, you can treat the latitude as constant.
EDIT: thinking about it I believe I will be stuck with the same problem: integrating a function that has a trigonometric function inside a square root.

Yeah I thought about it, but I had two different directions, but I wasn't sure if I could just use the arc length for the first equation, then for the second one and sum them over. Is that what I have to do? If it wasn't the case just to satisfy my curiosity how could I integrate the first function I posted?(My approximate scenario would also yield a function for the movement of a particle around a translating and rotating sphere, wouldn't it?).
 
I forgot to post how I solved the problem. I did the taylor series and then I integrated term by term. I did it a long time ago, but i forgott to post it here.
 
Something so thoughtful and sweet should have a place on the refrigerator forever! :smile:
 

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