Rotating reference frame

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A rotating frame of reference is a special case of a

inertial reference frame. An everyday example of a rotating reference frame is the surface of the Earth. (This article considers only frames rotating about a fixed axis. For more general rotations, see Euler angles
.)

In the inertial frame of reference (upper part of the picture), the black ball moves in a straight line. However, the observer (red dot) who is standing in the rotating/non-inertial frame of reference (lower part of the picture) sees the object as following a curved path due to the Coriolis and centrifugal forces present in this frame.

Fictitious forces

All non-inertial reference frames exhibit fictitious forces; rotating reference frames are characterized by three:[1]

and, for non-uniformly rotating reference frames,

Scientists in a rotating box can measure the

axis of rotation by measuring these fictitious forces. For example, Léon Foucault was able to show the Coriolis force that results from Earth's rotation using the Foucault pendulum. If Earth were to rotate many times faster, these fictitious forces could be felt by humans, as they are when on a spinning carousel
.

Centrifugal force

In

inertial forces), so named because, unlike real forces, they do not originate in interactions with other bodies situated in the environment of the particle upon which they act. Instead, centrifugal force originates in the rotation of the frame of reference within which observations are made.[2][3][4][5][6][7]

Coriolis force

The mathematical expression for the Coriolis force appeared in an 1835 paper by a French scientist

hydrodynamics, and also in the tidal equations of Pierre-Simon Laplace in 1778. Early in the 20th century, the term Coriolis force began to be used in connection with meteorology
.

Perhaps the most commonly encountered rotating reference frame is the

Coriolis effects in meteorology
).

Euler force

In classical mechanics, the Euler acceleration (named for Leonhard Euler), also known as azimuthal acceleration[8] or transverse acceleration[9] is an acceleration that appears when a non-uniformly rotating reference frame is used for analysis of motion and there is variation in the angular velocity of the reference frame's axis. This article is restricted to a frame of reference that rotates about a fixed axis.

The Euler force is a fictitious force on a body that is related to the Euler acceleration by F  = ma, where a is the Euler acceleration and m is the mass of the body.[10][11]

Relating rotating frames to stationary frames

The following is a derivation of the formulas for accelerations as well as fictitious forces in a rotating frame. It begins with the relation between a particle's coordinates in a rotating frame and its coordinates in an inertial (stationary) frame. Then, by taking time derivatives, formulas are derived that relate the velocity of the particle as seen in the two frames, and the acceleration relative to each frame. Using these accelerations, the fictitious forces are identified by comparing Newton's second law as formulated in the two different frames.

Relation between positions in the two frames

To derive these fictitious forces, it's helpful to be able to convert between the coordinates of the rotating reference frame and the coordinates of an

inertial reference frame with the same origin.[note 1]
If the rotation is about the axis with a constant angular velocity (so and which implies for some constant where denotes the angle in the -plane formed at time by and the -axis), and if the two reference frames coincide at time (meaning when so take or some other integer multiple of ), the transformation from rotating coordinates to inertial coordinates can be written
whereas the reverse transformation is

This result can be obtained from a rotation matrix.

Introduce the unit vectors representing standard unit basis vectors in the rotating frame. The time-derivatives of these unit vectors are found next. Suppose the frames are aligned at and the -axis is the axis of rotation. Then for a counterclockwise rotation through angle :

where the components are expressed in the stationary frame. Likewise,

Thus the time derivative of these vectors, which rotate without changing magnitude, is

where This result is the same as found using a
vector cross product
with the rotation vector pointed along the z-axis of rotation namely,
where is either or

Time derivatives in the two frames

Introduce unit vectors , now representing standard unit basis vectors in the general rotating frame. As they rotate they will remain normalized and perpendicular to each other. If they rotate at the speed of about an axis along the rotation vector then each unit vector of the rotating coordinate system (such as or ) abides by the following equation:

So if denotes the transformation taking basis vectors of the inertial- to the rotating frame, with matrix columns equal to the basis vectors of the rotating frame, then the cross product multiplication by the rotation vector is given by .

If is a vector function that is written as[note 2]

and we want to examine its first derivative then (using the product rule of differentiation):[12][13]
where denotes the rate of change of as observed in the rotating coordinate system. As a shorthand the differentiation is expressed as:

This result is also known as the transport theorem in analytical dynamics and is also sometimes referred to as the basic kinematic equation.[14]

Relation between velocities in the two frames

A velocity of an object is the time-derivative of the object's position, so

The time derivative of a position in a rotating reference frame has two components, one from the explicit time dependence due to motion of the object itself in the rotating reference frame, and another from the frame's own rotation. Applying the result of the previous subsection to the displacement the velocities in the two reference frames are related by the equation

where subscript means the inertial frame of reference, and means the rotating frame of reference.

Relation between accelerations in the two frames

Acceleration is the second time derivative of position, or the first time derivative of velocity

where subscript means the inertial frame of reference, the rotating frame of reference, and where the expression, again, in the bracketed expression on the left is to be interpreted as an operator working onto the bracketed expression on the right.

As , the first time derivatives of inside either frame, when expressed with respect to the basis of e.g. the inertial frame, coincide. Carrying out the differentiations and re-arranging some terms yields the acceleration relative to the rotating reference frame,

where is the apparent acceleration in the rotating reference frame, the term represents

centrifugal acceleration
, and the term is the
Coriolis acceleration
. The last term, , is the
Euler acceleration
and is zero in uniformly rotating frames.

Newton's second law in the two frames

When the expression for acceleration is multiplied by the mass of the particle, the three extra terms on the right-hand side result in fictitious forces in the rotating reference frame, that is, apparent forces that result from being in a non-inertial reference frame, rather than from any physical interaction between bodies.

Using Newton's second law of motion we obtain:[1][12][13][15][16]

  • the Coriolis force
  • the
    centrifugal force
  • and the Euler force

where is the mass of the object being acted upon by these fictitious forces. Notice that all three forces vanish when the frame is not rotating, that is, when

For completeness, the inertial acceleration due to impressed external forces can be determined from the total physical force in the inertial (non-rotating) frame (for example, force from physical interactions such as electromagnetic forces) using Newton's second law in the inertial frame:

Newton's law in the rotating frame then becomes

In other words, to handle the laws of motion in a rotating reference frame:[16][17][18]

Treat the fictitious forces like real forces, and pretend you are in an inertial frame.

— Louis N. Hand, Janet D. Finch Analytical Mechanics, p. 267

Obviously, a rotating frame of reference is a case of a non-inertial frame. Thus the particle in addition to the real force is acted upon by a fictitious force...The particle will move according to Newton's second law of motion if the total force acting on it is taken as the sum of the real and fictitious forces.

— HS Hans & SP Pui: Mechanics; p. 341

This equation has exactly the form of Newton's second law, except that in addition to F, the sum of all forces identified in the inertial frame, there is an extra term on the right...This means we can continue to use Newton's second law in the noninertial frame provided we agree that in the noninertial frame we must add an extra force-like term, often called the inertial force.

— John R. Taylor: Classical Mechanics; p. 328

Use in magnetic resonance

It is convenient to consider

rotating wave approximation
may also be used.

Animation showing the rotating frame. The red arrow is a spin in the Bloch sphere which precesses in the laboratory frame due to a static magnetic field. In the rotating frame the spin remains still until a resonantly oscillating magnetic field drives magnetic resonance.

See also

References

  1. ^ .
  2. .
  3. .
  4. .
  5. .
  6. ^ David McNaughton. "Centrifugal and Coriolis Effects". Retrieved 2008-05-18.
  7. ^ David P. Stern. "Frames of reference: The centrifugal force". Retrieved 2008-10-26.
  8. . acceleration azimuthal Morin.
  9. ^ Grant R. Fowles & George L. Cassiday (1999). Analytical Mechanics (6th ed.). Harcourt College Publishers. p. 178.
  10. .
  11. .
  12. ^ .
  13. ^ .
  14. ^ Corless, Martin. "Kinematics" (PDF). Aeromechanics I Course Notes. Purdue University. p. 213. Archived from the original (PDF) on 24 October 2012. Retrieved 18 July 2011.
  15. .
  16. ^ .
  17. .
  18. .
  1. ^ So are functions of and time Similarly are functions of and That these reference frames have the same origin means that for all if and only if
  2. ^ So are 's coordinates with respect to the rotating basis vector ('s coordinates with respect to the inertial frame are not used). Consequently, at any given instant, the rate of change of with respect to these rotating coordinates is So for example, if and are constants, then is just one of the rotating basis vectors and (as expected) its time rate of change with respect to these rotating coordinates is identically (so the formula for given below implies that the derivative at time of this rotating basis vector is ); however, its rate of change with respect to the non-rotating inertial frame will not be constantly except (of course) in the case where is not moving in the inertial frame (this happens, for instance, when the axis of rotation is fixed as the -axis (assuming standard coordinates) in the inertial frame and also or ).

External links

  • Animation clip showing scenes as viewed from both an inertial frame and a rotating frame of reference, visualizing the Coriolis and centrifugal forces.