Modelling the motion of a meteor

Click For Summary
SUMMARY

The discussion focuses on modeling the motion of a meteor through the atmosphere, specifically addressing mass loss upon impact (0.025 kg) and the effects of air resistance, which varies with height. The participant seeks assistance in numerically solving the differential equations for the meteor's trajectory, x(t) and y(t), using initial conditions. Key insights include the recommendation to utilize MATLAB for numerical solutions and the suggestion to start with simple integration techniques before advancing to more complex methods.

PREREQUISITES
  • Understanding of ordinary differential equations (ODEs)
  • Familiarity with numerical integration techniques
  • Knowledge of atmospheric physics, particularly air density variations
  • Proficiency in MATLAB for computational modeling
NEXT STEPS
  • Research numerical methods for solving ordinary differential equations in MATLAB
  • Explore the impact of air resistance on projectile motion
  • Study the relationship between atmospheric density and altitude
  • Learn about different integration schemes, such as Euler's method and Runge-Kutta methods
USEFUL FOR

Students in physics or engineering fields, educators teaching dynamics, and anyone interested in computational modeling of atmospheric phenomena.

PeterH
Messages
16
Reaction score
0
Hi!
I am to model the motion of a meteor as it travels through the atmosphere, taking into account the loss of mass, which is 0.025 kg upon impact (height = 0). I also have to take into account the air resistance on the meteor, the fact that the air density is a function of height and that the orthographic projection of the meteor perpendicular the direction of movement (part of the air resistance equation) is a function of the mass of the meteor.
I assume that gravitational field strength is constant.

I have attached a picture of the equations I have been able to derive so far using standard formulas.

I have to solve the differential equations for x(t) and y(t) numerically, however, I fail to see how and therefore seek help.

This is for a very important school project and I'm running out of time, so I really need help. Even the smallest hint would be greatly appreciated!
 

Attachments

  • Mat.jpg
    Mat.jpg
    40.6 KB · Views: 514
Physics news on Phys.org
Simply calculate it step by step in small time steps?
You know the initial position and velocity at t=0, you can calculate the acceleration there and use this to estimate the position and velocity at t=0.01s (or whatever). Use the data there to estimate the values for t=0.02s and so on. There are better integration schemes, but start with the easiest one and improve that later if you like.

Your equation for A can be simplified a bit.

The atmospheric density does not follow an exponential law as the temperature depends on height, by the way.
 
Newtonian gravity with atmospheric drag is not solvable analytically. Use an ordinary differential equation numerical solver. I prefer MATLAB.

It would help if you tell us what exactly A(m), m(t), etc are. Also, what is that little squiggly variable for? Is it a constant?
 
Last edited:
This is everything
 

Attachments

  • Mat.jpg
    Mat.jpg
    28.3 KB · Views: 492
Mass as a function of time only
 

Attachments

  • Mass.jpg
    Mass.jpg
    5.6 KB · Views: 539
I don't think that equation for m(t) makes sense, it has m(t) at the right side as well, but multiplied by t and other factors. Looks like a wrong differential equation.
 

Similar threads

  • · Replies 3 ·
Replies
3
Views
2K
  • · Replies 1 ·
Replies
1
Views
2K
  • · Replies 1 ·
Replies
1
Views
1K
  • · Replies 15 ·
Replies
15
Views
1K
  • · Replies 3 ·
Replies
3
Views
2K
  • · Replies 17 ·
Replies
17
Views
2K
  • · Replies 6 ·
Replies
6
Views
4K
  • · Replies 1 ·
Replies
1
Views
5K
  • · Replies 8 ·
Replies
8
Views
2K
  • · Replies 2 ·
Replies
2
Views
2K