In classical mechanics, the Newton–Euler equations describe the combined translational and rotational dynamics of a rigid body.
Traditionally the Newton–Euler equations is the grouping together of Euler's two laws of motion for a rigid body into a single equation with 6 components, using column vectors and matrices. These laws relate the motion of the center of gravity of a rigid body with the sum of forces and torques (or synonymously moments) acting on the rigid body.
Center of mass frame With respect to a coordinate frame whose origin coincides with the body's center of mass for τ(torque) and an inertial frame of reference for F(force), they can be expressed in matrix form as:
( F τ ) = ( m I 3 0 0 I c m ) ( a c m α ) + ( 0 ω × ( I c m ω ) ) , {\displaystyle \left({\begin{matrix}{\mathbf {F} }\\{\boldsymbol {\tau }}\end{matrix}}\right)=\left({\begin{matrix}m{\mathbf {I} _{3}}&0\\0&{\mathbf {I} }_{\rm {cm}}\end{matrix}}\right)\left({\begin{matrix}\mathbf {a} _{\rm {cm}}\\{\boldsymbol {\alpha }}\end{matrix}}\right)+\left({\begin{matrix}0\\{\boldsymbol {\omega }}\times \left({\mathbf {I} }_{\rm {cm}}\,{\boldsymbol {\omega }}\right)\end{matrix}}\right),}
where
F = total force acting on the center of mass m = mass of the body I3 = the 3×3 identity matrix acm = acceleration of the center of mass vcm = velocity of the center of mass τ = total torque acting about the center of mass Icm = moment of inertia about the center of mass ω = angular velocity of the body α = angular acceleration of the body
Arbitrary reference frame With respect to a coordinate frame located at point P that is fixed in the body and not coincident with the center of mass, the equations assume the more complex form:
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