Rotating reference frame
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A rotating frame of reference is a special case of a non-inertial reference frame in which the coordinate system is rotating relative to an inertial reference frame. An everyday example of a rotating reference frame is the surface of the Earth.
Fictitious forces
All non-inertial reference frames exhibit fictitious forces. Rotating reference frames are characterized by three fictitious forces
- the centrifugal force
- the Coriolis force
- the Euler force.
Relation between positions in the two frames
To derive these fictitious forces, it's helpful to be able to convert between the coordinates [\left( x^,y^,z^ \right)] of the rotating reference frame and the coordinates [\left( x, y, z \right)] of an inertial reference frame with the same origin. If the rotation is about the [z] axis with an angular velocity [\omega] and the two reference frames coincide at time [t=0], the transformation from rotating coordinates to inertial coordinates can be written
- [x = x^\ \cos\omega t + y^\ \sin\omega t]
- [y = y^\ \cos\omega t - x^\ \sin\omega t]
- [x^ = x\ \cos\left(-\omega t\right) - y\ \sin\left( -\omega t \right)]
- [y^ = y\ \cos\left( -\omega t \right) + x\ \sin\left( -\omega t \right)]
Relation between velocities in the two frames
A velocity of an object is the time-derivative of the object's position, or
- [\mathbf \equiv \frac}]
- [ \left( \frac \right)_} = \left( \frac \right)_} + \boldsymbol\omega \times ]
- [ \mathbf_} \equiv \left( \frac} \right)_} = \left( \frac} \right)_} + \boldsymbol\omega \times \mathbf = \mathbf_} + \boldsymbol\omega \times \mathbf]
Relation between accelerations in the two frames
Acceleration is the second time derivative of position, or the first time derivative of velocity
- [ \mathbf_} \equiv \left( \frac\mathbf}}\right)_} = \left( \frac} \right)_} = \left[ left( frac right)_} + boldsymbolomega times right]\left[left( frac} right)_} + boldsymbolomega times mathbf right] ]
- [ \mathbf_} = \mathbf_} - 2 \boldsymbol\omega \times \mathbf_} - \boldsymbol\omega \times \boldsymbol\omega \times \mathbf - \frac \times \mathbf]
The three extra terms on the right-hand side result in fictitious forces in the rotating reference frame, i.e., accelerations that result from being in a non-inertial reference frame, rather than from any physical force. Using Newton's second law of motion [F=ma], we obtain
- the Coriolis force
- [\mathbf_} = -2m \boldsymbol\omega \times \mathbf_}]
- [\mathbf_} = -m\boldsymbol\omega \times \boldsymbol\omega \times \mathbf]
- and the Euler force
- [\mathbf_} = -m\frac \times \mathbf]
For completeness, the inertial acceleration [\mathbf_}] can be determined from the total physical force [\mathbf_}] (i.e., the total force from physical interactions such as electromagnetism) likewise using Newton's second law
- [\mathbf_} = m \mathbf_}]
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