Part of a series on
Classical mechanics
${\displaystyle {\textbf {F}}={\frac {d\mathbf {p} }{dt}}}$ Second law of motion
History Timeline Textbooks
Branches Applied Celestial Continuum Dynamics Field theory Kinematics Kinetics Statics Statistical mechanics
Fundamentals Acceleration Angular momentum Couple D'Alembert's principle Energy kinetic potential Force Frame of reference Inertial frame of reference Impulse Inertia / Moment of inertia Mass Mechanical power Mechanical work Moment Momentum Space Speed Time Torque Velocity Virtual work
Formulations Newton's laws of motion Analytical mechanics Lagrangian mechanics Hamiltonian mechanics Routhian mechanics Hamilton–Jacobi equation Appell's equation of motion Koopman–von Neumann mechanics
Core topics Damping Displacement Equations of motion Euler's laws of motion Fictitious force Friction Harmonic oscillator Inertial / Non-inertial reference frame Motion (linear) Newton's law of universal gravitation Newton's laws of motion Relative velocity Rigid body dynamics Euler's equations Simple harmonic motion Vibration
Rotation Circular motion Rotating reference frame Centripetal force Centrifugal force reactive Coriolis force Pendulum Tangential speed Rotational frequency Angular acceleration / displacement / frequency / velocity
Scientists Kepler Galileo Huygens Newton Horrocks Halley Maupertuis Daniel Bernoulli Johann Bernoulli Euler d'Alembert Clairaut Lagrange Laplace Poisson Hamilton Jacobi Cauchy Routh Liouville Appell Gibbs Koopman von Neumann
Physics portal  Category
v t e

In classical mechanics, Euler's rotation equations are a vectorial quasilinear first-order ordinary differential equation describing the rotation of a rigid body, using a rotating reference frame with angular velocity ω whose axes are fixed to the body. They are named in honour of Leonhard Euler. Their general vector form is

${\displaystyle \mathbf {I} {\dot {\boldsymbol {\omega }}}+{\boldsymbol {\omega }}\times \left(\mathbf {I} {\boldsymbol {\omega }}\right)=\mathbf {M} .}$

where M is the applied torques and I is the inertia matrix. The vector ${\displaystyle {\dot {\boldsymbol {\omega }}}}$ is the angular acceleration. Again, note that all quantities are defined in the rotating reference frame.

In orthogonal principal axes of inertia coordinates the equations become

${\displaystyle {\begin{aligned}I_{1}\,{\dot {\omega }}_{1}+(I_{3}-I_{2})\,\omega _{2}\,\omega _{3}&=M_{1}\\I_{2}\,{\dot {\omega }}_{2}+(I_{1}-I_{3})\,\omega _{3}\,\omega _{1}&=M_{2}\\I_{3}\,{\dot {\omega }}_{3}+(I_{2}-I_{1})\,\omega _{1}\,\omega _{2}&=M_{3}\end{aligned}}}$

where M_k are the components of the applied torques, I_k are the principal moments of inertia and ω_k are the components of the angular velocity.

In the absence of applied torques, one obtains the Euler top. When the torques are due to gravity, there are special cases when the motion of the top is integrable.

In an inertial frame of reference (subscripted "in"), Euler's second law states that the time derivative of the angular momentum L equals the applied torque:

${\displaystyle {\frac {d\mathbf {L} _{\text{in}}}{dt}}=\mathbf {M} _{\text{in}}}$

For point particles such that the internal forces are central forces, this may be derived using Newton's second law. For a rigid body, one has the relation between angular momentum and the moment of inertia I_in given as

${\displaystyle \mathbf {L} _{\text{in}}=\mathbf {I} _{\text{in}}{\boldsymbol {\omega }}}$

In the inertial frame, the differential equation is not always helpful in solving for the motion of a general rotating rigid body, as both I_in and ω can change during the motion. One may instead change to a coordinate frame fixed in the rotating body, in which the moment of inertia tensor is constant. Using a reference frame such as that at the center of mass, the frame's position drops out of the equations. In any rotating reference frame, the time derivative must be replaced so that the equation becomes

${\displaystyle \left({\frac {d\mathbf {L} }{dt}}\right)_{\mathrm {rot} }+{\boldsymbol {\omega }}\times \mathbf {L} =\mathbf {M} }$

and so the cross product arises, see time derivative in rotating reference frame. The vector components of the torque in the inertial and the rotating frames are related by ${\displaystyle \mathbf {M} _{\text{in}}=\mathbf {Q} \mathbf {M} ,}$ where ${\displaystyle \mathbf {Q} }$ is the rotation tensor (not rotation matrix), an orthogonal tensor related to the angular velocity vector by ${\displaystyle {\boldsymbol {\omega }}\times {\boldsymbol {u}}={\dot {\mathbf {Q} }}\mathbf {Q} ^{-1}{\boldsymbol {u}}}$ for any vector u. Now ${\displaystyle \mathbf {L} =\mathbf {I} {\boldsymbol {\omega }}}$ is substituted and the time derivatives are taken in the rotating frame, while realizing that the particle positions and the inertia tensor does not depend on time. This leads to the general vector form of Euler's equations which are valid in such a frame

${\displaystyle \mathbf {I} {\dot {\boldsymbol {\omega }}}+{\boldsymbol {\omega }}\times \left(\mathbf {I} {\boldsymbol {\omega }}\right)=\mathbf {M} .}$

The equations are also derived from Newton's laws in the discussion of the resultant torque.

More generally, by the tensor transform rules, any rank-2 tensor ${\displaystyle \mathbf {T} }$ has a time-derivative ${\displaystyle \mathbf {\dot {T}} }$ such that for any vector ${\displaystyle \mathbf {u} }$, one has ${\displaystyle \mathbf {\dot {T}} \mathbf {u} ={\boldsymbol {\omega }}\times (\mathbf {T} \mathbf {u} )-\mathbf {T} ({\boldsymbol {\omega }}\times \mathbf {u} )}$. This yields the Euler's equations by plugging in ${\displaystyle {\frac {d}{dt}}\left(\mathbf {I} {\boldsymbol {\omega }}\right)=\mathbf {M} .}$

When choosing a frame so that its axes are aligned with the principal axes of the inertia tensor, its component matrix is diagonal, which further simplifies calculations. As described in the moment of inertia article, the angular momentum L can then be written

${\displaystyle \mathbf {L} =L_{1}\mathbf {e} _{1}+L_{2}\mathbf {e} _{2}+L_{3}\mathbf {e} _{3}=\sum _{i=1}^{3}I_{i}\omega _{i}\mathbf {e} _{i}}$

Also in some frames not tied to the body can it be possible to obtain such simple (diagonal tensor) equations for the rate of change of the angular momentum. Then ω must be the angular velocity for rotation of that frames axes instead of the rotation of the body. It is however still required that the chosen axes are still principal axes of inertia. The resulting form of the Euler rotation equations is useful for rotation-symmetric objects that allow some of the principal axes of rotation to be chosen freely.

Torque-free precessions are non-trivial solution for the situation where the torque on the right hand side is zero. When I is not constant in the external reference frame (i.e. the body is moving and its inertia tensor is not constantly diagonal) then I cannot be pulled through the derivative operator acting on L. In this case I(t) and ω(t) do change together in such a way that the derivative of their product is still zero. This motion can be visualized by Poinsot's construction.

The Euler equations can be generalized to any simple Lie algebra.^[1] The original Euler equations come from fixing the Lie algebra to be ${\displaystyle {\mathfrak {so}}(3)}$, with generators ${\displaystyle {t_{1},t_{2},t_{3}}}$ satisfying the relation ${\displaystyle [t_{a},t_{b}]=\epsilon _{abc}t_{c}}$. Then if ${\displaystyle {\boldsymbol {\omega }}(t)=\sum _{a}\omega _{a}(t)t_{a}}$ (where ${\displaystyle t}$ is a time coordinate, not to be confused with basis vectors ${\displaystyle t_{a}}$) is an ${\displaystyle {\mathfrak {so}}(3)}$-valued function of time, and ${\displaystyle \mathbf {I} =\mathrm {diag} (I_{1},I_{2},I_{3})}$ (with respect to the Lie algebra basis), then the (untorqued) original Euler equations can be written^[2] $${\displaystyle \mathbf {I} {\dot {\boldsymbol {\omega }}}=[\mathbf {I} {\boldsymbol {\omega }},{\boldsymbol {\omega }}].}$$ To define ${\displaystyle \mathbf {I} }$ in a basis-independent way, it must be a self-adjoint map on the Lie algebra ${\displaystyle {\mathfrak {g}}}$ with respect to the invariant bilinear form on ${\displaystyle {\mathfrak {g}}}$. This expression generalizes readily to an arbitrary simple Lie algebra, say in the standard classification of simple Lie algebras.

This can also be viewed as a Lax pair formulation of the generalized Euler equations, suggesting their integrability.

• Euler angles
• Dzhanibekov effect
• Moment of inertia
• Poinsot's ellipsoid
• Rigid rotor

• C. A. Truesdell, III (1991) A First Course in Rational Continuum Mechanics. Vol. 1: General Concepts, 2nd ed., Academic Press. ISBN 0-12-701300-8. Sects. I.8-10.
• C. A. Truesdell, III and R. A. Toupin (1960) The Classical Field Theories, in S. Flügge (ed.) Encyclopedia of Physics. Vol. III/1: Principles of Classical Mechanics and Field Theory, Springer-Verlag. Sects. 166–168, 196–197, and 294.
• Landau L.D. and Lifshitz E.M. (1976) Mechanics, 3rd. ed., Pergamon Press. ISBN 0-08-021022-8 (hardcover) and ISBN 0-08-029141-4 (softcover).
• Goldstein H. (1980) Classical Mechanics, 2nd ed., Addison-Wesley. ISBN 0-201-02918-9
• Symon KR. (1971) Mechanics, 3rd. ed., Addison-Wesley. ISBN 0-201-07392-7