Equations of Motion for 'Perturbed' Or 'Oblique Incidence' Orbits?

In summary, to derive the equation of motion for an oblique incidence particle undergoing circular/near-circular motion in an electric field that varies as 1/r, you can use Newton's Second Law and the equation F = qE to calculate the net force and acceleration of the particle.
  • #1
Physics Enemy
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Hi,

I've been doing a Q where particles undergo circular/near-circular motion in an electric field. The electric field varies as 1/r. With the first particle, they set it off tangentially to the field lines, so it undergoes circular motion.

With the second particle, they set it off at a slight deviation from the tangential line. I figured, also from their diagram, the orbit would look slightly elliptical, perhaps still close to circular.

How do I go about deriving an equation of motion for this 'oblique incidence' particle? My only thoughts at this stage are that the force on the particle varies, since it's radial distance varies, unlike with circular motion.

What does it actually want me to do though?

Thanks!
 
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  • #2
The equation of motion for this oblique incidence particle can be derived by using Newton's Second Law. This law states that the net force acting on an object is equal to its mass multiplied by its acceleration. Therefore, you can calculate the net force on the particle by taking the derivative of its velocity with respect to time. The electric field will provide a force in the radial direction, and this can be calculated using the equation F = qE, where q is the charge of the particle and E is the electric field. You can then use this to determine the acceleration of the particle, which can then be used to calculate its equation of motion.
 

What are perturbed orbits?

Perturbed orbits are orbits that are affected by external forces or influences, such as gravitational pull from other bodies or atmospheric drag. These forces cause the orbit to deviate from its ideal shape and trajectory.

What is oblique incidence in relation to orbits?

Oblique incidence refers to the angle at which a body or object enters into an orbit. In other words, it is the angle between the direction of motion and the tangent to the orbit at the point of entry. This angle can greatly affect the trajectory and stability of the orbit.

How do equations of motion for perturbed orbits differ from those for ideal orbits?

The equations of motion for perturbed orbits take into account the external forces and influences that affect the orbit, while equations for ideal orbits assume a perfectly symmetrical and stable orbit. This means that the equations for perturbed orbits are more complex and may involve additional variables and adjustments.

What factors can perturb an orbit?

There are several factors that can perturb an orbit, including gravitational pull from other bodies, atmospheric drag, and irregularities in the shape of the orbit. Other factors such as solar radiation pressure and the oblateness of Earth can also play a role in perturbing orbits.

How are perturbed orbits calculated and predicted?

Perturbed orbits are typically calculated and predicted using numerical methods and computer simulations. These take into account the various external forces and influences on the orbit and calculate the resulting trajectory. These calculations can also be adjusted and refined as more data and observations become available.

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