TOPICS
Search

Euler's Equations of Rigid Body Motion


Euler's equations of rigid body motion are ordinary differential equations for the components omega_1, omega_2, and omega_3 of angular velocity in a frame attached to a rigid body. Choose the principal axes of the moment of inertia about its center of mass, and let I_1, I_2, and I_3 be the corresponding positive moments. If tau_i are the components of the applied torque about the center of mass, then

I_1omega^._1=(I_2-I_3)omega_2omega_3+tau_1
(1)
I_2omega^._2=(I_3-I_1)omega_3omega_1+tau_2
(2)
I_3omega^._3=(I_1-I_2)omega_1omega_2+tau_3.
(3)

The same equations apply to rotation about a fixed point when the moments and torques are taken about that point (Peraire and Widnall 2009, pp. 1-3).

For torque-free motion, the rotational kinetic energy T=1/2sum_(i=1)^(3)I_iomega_i^2 and the squared magnitude of the angular momentum L^2=sum_(i=1)^(3)I_i^2omega_i^2 are integrals of motion. These invariants and the linear stability of rotation about each principal axis give the intermediate axis theorem.


See also

Angular Velocity, Integral of Motion, Intermediate Axis Theorem, Moment of Inertia, Ordinary Differential Equation, Principal Axis

Explore with Wolfram|Alpha

References

Peraire, J. and Widnall, S. "3D Rigid Body Dynamics: Equations of Motion; Euler's Equations." Lecture 28 in 16.07 Dynamics. MIT OpenCourseWare, 2009. https://ocw.mit.edu/courses/16-07-dynamics-fall-2009/5e1d8699338146e5127080b880b906d6_MIT16_07F09_Lec28.pdf.

Cite this as:

Weisstein, Eric W. "Euler's Equations of Rigid Body Motion." From MathWorld--A Wolfram Resource. https://mathworld.wolfram.com/EulersEquationsofRigidBodyMotion.html

Subject classifications