Two-dimensional motion under Central Force

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SUMMARY

The discussion focuses on the analysis of particle motion under a central force, specifically examining the equations for x(t) and y(t) defined as x(t) = A [ kt – cos(βt) ] and y(t) = B [ 1 – sin(βt) ]. Participants aim to determine the radial and tangential orbital velocities, assuming an elliptical orbit, and to recover the canonical form of the equation (x²/a² + y²/b² = 1). The complexity of deriving these velocities and the challenges in eliminating time from the equations are highlighted, with suggestions of potential parabolic solutions rather than elliptical orbits.

PREREQUISITES
  • Understanding of central force motion in physics
  • Familiarity with parametric equations and their derivatives
  • Knowledge of elliptical and parabolic orbits
  • Basic skills in coordinate transformations
NEXT STEPS
  • Study the derivation of radial and tangential velocities in central force problems
  • Learn about coordinate transformations in motion analysis
  • Explore the characteristics of parabolic versus elliptical orbits
  • Investigate the implications of unbounded motion in central force systems
USEFUL FOR

Students and educators in physics, particularly those focusing on classical mechanics and orbital dynamics, will benefit from this discussion.

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Homework Statement



Some students have just drawn my attention to the problem of particle motion under central force where the x and y coordinates are specified as functions of time, such as

x(t) = A [ kt – cos(βt) ]
y(t) = B [ 1 – sin(βt) ],

(here A, B, β and k are constants).




Homework Equations



The problem is to determine the radial and tangential orbital velocities (orbit assumed to be elliptical), and recover the canonical form of the equation (x2/a2 + y2/b2 = 1).
I have tried to figure this out for a few days without much success. Can anyone assist please?



The Attempt at a Solution



Express position vector r as

r = [x2 + y2]1/2
and evaluate dr/dt to obtain velocity as function of t. But this leads to messy calculation, which does not yield the angular and radial dependence.

Equally, attempt to eliminate t and obtain an equation in x and y proves quite hard.

We have also thought of coordinate transformation from (x,y,a,b) to (u,v,c,d) where u,v are velocity axes, but could not quite effect that.

 
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Since x(t) is unbounded, this doesn't look like a closed orbit. It's possible that this is a parabolic solution to a central force law, but you might want to verify that.
 
Thanks, very much, fzero, for early intervention.

I agree entirely that the orbit may not be elliptical!
 

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