Modeling an Asteroid's Trajectory Towards the Sun Using Differential Equations

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Homework Help Overview

The discussion revolves around modeling the trajectory of an asteroid falling towards the sun using differential equations. The original poster outlines a problem involving the derivation of a differential equation for the position of the asteroid as a function of time and the subsequent solution for time as a function of position.

Discussion Character

  • Exploratory, Mathematical reasoning, Assumption checking

Approaches and Questions Raised

  • Participants discuss the formulation of the differential equation based on Newton's second law and explore the integration of velocity with respect to position. There are questions regarding the correctness of signs and the treatment of limits during integration. Some participants express uncertainty about the mathematical steps taken and whether they are on the right track.

Discussion Status

There is an ongoing exploration of the integration process and its implications for the equations being derived. Some participants have offered guidance on the correct approach to integration and the need for careful consideration of signs. The discussion reflects a mix of attempts to clarify misunderstandings and to refine the mathematical expressions involved.

Contextual Notes

Participants note the complexity of the integral involved and the challenges of ensuring mathematical correctness throughout the derivation process. There are also references to the potential for infinite limits in the context of the problem, indicating a need for careful handling of assumptions and conditions in the model.

  • #31
OK thanks! Well if all else fails I'm pretty sure I have the other 4 parts of the question right.

The more I think about it the more reasonable I guess it could be since it is starting from a stop from such a long ways away. It's initial acceleration is soooo tiny. I guess it would hang around the Kuiper belt for a very long time before it gained any appreciable speed.
 
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  • #32
I got even more, but now I am sleepy. Try the approximation of E=0, and getting v from conservation of energy. It is much easier.
By the way, did you set your calculator to RAD when calculating the arctan(1/29)?
 
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  • #33
I got using both methods that the speed of the asteroid as it passes Earth is about 1300 km/s. One way I got 1311 and another 1333 km/s.

I don't know how you get time from there though. Since the acceleration isn't constant I obviously can't use a kinematic equation or anything.
 
  • #34
You get v(t) = -dr/dt from conservation of energy. Need integral, but it is easy.
 
  • #35
Hrm, doing it with energy (if I did it right) I get 12.3 years.

I used

1/2 mv^2 = \frac{GMm}{r}

turned that into

-dr/dt = \sqrt{\frac{2GM}{r}}

I integrate from R to r and 0 to t

I get

t = 2/3 * \frac{R^{1.5}-r^{1.5}}{\sqrt{2GM}}
 
  • #36
It looks good. What did you get for t?
 
  • #37
I get 12.3 years from that. I had 29 years the other way. But the other way was much more mistake prone.
 
  • #38
Crush1986 said:
I get 12.3 years from that. I had 29 years the other way. But the other way was much more mistake prone.
Yes, it was easy to make mistakes, but I got the same results as you at the end. The initial conditions were different. The first method assumed zero initial speed, negative total energy. The second one assumed zero total energy, but that meant nonzero initial speed. As you noticed, the asteroid gains speed very slowly at the beginning. That can cause the difference between the times.
 
  • #39
ehild said:
Yes, it was easy to make mistakes, but I got the same results as you at the end. The initial conditions were different. The first method assumed zero initial speed, negative total energy. The second one assumed zero total energy, but that meant nonzero initial speed. As you noticed, the asteroid gains speed very slowly at the beginning. That can cause the difference between the times.
I see. If we made crude approximations that the P.E. at this distance is zero, and assumed the asteroid had zero speed at it's beginning. Method 2 would be ok, right?
 
  • #40
Crush1986 said:
I see. If we made crude approximations that the P.E. at this distance is zero, and assumed the asteroid had zero speed at it's beginning. Method 2 would be ok, right?
Both methods have sense. The complicated one assumed that the asteroid had zero speed, so its energy was negative. The simple method assumed zero total energy, which meant it got some initial speed towards the Sun.
The spaceship New Horizons arrived to Pluto in about 9 years, in a backward track. http://pluto.jhuapl.edu/Mission/The-Path-to-Pluto/Mission-Timeline.php. So times of a few decades have sense.
 
  • #41
I see thanks!

This problem definitely showed me a lot of things I have to learn. I was completely taken by surprise by the negative differentials. I guess it makes sense though, if the force is attractive it's negative, so the acceleration has to be negative. As a consequence dr/dt is also negative with how the problem is describing what the asteroid is doing.
 
  • #42
The velocity and acceleration are first and second time derivatives of the position vector. Putting the origin into the sun, ##\vec v = \frac{d \vec r }{dt}##. But we worked with the scalar r, distance between Sun and asteroid. It decreased with time. That is why we used the negative sign: v, the speed was v=-dr/dt.
 
  • #43
Hrm, ok. I think that is how I was thinking about it. I just said it horribly. I think I understand all that went on in here, haha. I'm definitely going to be mulling it over at work tonight. Thanks! Hopefully all this time will greatly increase my understanding.
 

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