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Euler's equations with torque for the rigid-material model, the rotational power identity, the torque-free reduction and frame covariance

Physical scope

Conditional deductions inside the external-torque branch of Adoption of the external-torque branch of the rigid-material model: declared torque data and the balance of angular momentum about the centre of mass for the rigid-material model of Adoption of the rigid-material model branch: reference mass distribution, rigid placements, orientation and scope: the body-frame Euler equations with the declared torque datum, their principal-axis components, the power identity ddt12ωTIω=ω⋅RTτ (and constancy of the rotational kinetic energy in the torque-free case), the torque-free reduction l′=l×(I−1l) under nondegeneracy, and the preservation of the balance under changes of inertial frame with the declared transformation of the torque datum. No force law producing τ, no conservation of Lc (which is proved on the same page), no measurement and no empirical value is asserted.

Statement

Assume the Axiom of Countable Choice ACω (The Axiom of Countable Choice (ACω)), used only through the integrals of Total momentum, kinetic-energy splitting and centre-of-mass angular momentum of a rigid-material motion; the theorems below neither use nor imply any other choice principle. Adopt a model of the rigid-material branch Adoption of the rigid-material model branch: reference mass distribution, rigid placements, orientation and scope with the external-torque branch Adoption of the external-torque branch of the rigid-material model: declared torque data and the balance of angular momentum about the centre of mass: a reference mass distribution ν with total mass m and centred reference coordinates, a time window I0 (Intervals of R: the nine order-convex forms, nondegeneracy, and length), an inertial frame, a motion x(t,ρ)=c(t)+R(t)ρ with configuration path (c,R) of class C2 (Configuration, configuration space and orientation of a rigid-material model in an inertial frame), body angular velocity ω (Body and spatial angular velocity of a rigid-material motion, and the material velocity field) and body inertia matrix I (Inertia matrix, spatial inertia tensor, inertia tensor about a point and moment of inertia about an axis of a rigid-material model), and a continuous external torque datum τ:I0→R3 with respect to which the adopted balance of Adoption of the external-torque branch of the rigid-material model: declared torque data and the balance of angular momentum about the centre of mass clause (iii) holds along the motion. Then:

  1. Euler's equations with torque. Writing l:=Iω, one has l′=RTτ−ω×Iω and Iω′(t)+ω(t)×Iω(t)=R(t)Tτ(t)(t∈I0).
  2. Principal-axis components. If (e1,e2,e3) is a positively oriented orthonormal eigenbasis of I with Iej=Ijej (Principal axes and principal moments of the inertia data of a rigid-material model, axis moments and extremal values clause (a)) and ω=∑jωjej, RTτ=∑jτjej, then the equations are componentwise I1ω1′=(I2−I3)ω2ω3+τ1,I2ω2′=(I3−I1)ω3ω1+τ2,I3ω3′=(I1−I2)ω1ω2+τ3.
  3. Rotational power identity. The rotational kinetic energy Krot(t):=12ω(t)TIω(t) is differentiable on I0 with ddtKrot(t)=ω(t)⋅R(t)Tτ(t)(t∈I0); in particular, if τ≡0, then Krot is constant on I0, and Krot coincides with the rotational term 12ωTIω of the model's kinetic energy in clause 3 of Total momentum, kinetic-energy splitting and centre-of-mass angular momentum of a rigid-material motion.
  4. Torque-free reduction and nondegeneracy. Suppose τ≡0 and the model is nondegenerate in the sense of Inertia matrix, spatial inertia tensor, inertia tensor about a point and moment of inertia about an axis of a rigid-material model clause (a), so that I is invertible with I−1l=ω. Then, writing ω as a function of l, l′=l×(I−1l),ω′=F(ω):=−I−1(ω×Iω); the second form exhibits the torque-free body angular velocity as a solution of the autonomous field F on R3.
  5. Frame covariance. Let a second inertial frame be related to the first by t′=t+b, x′=Qx+ut+a with b∈R, a,u∈R3, Q∈SO(3) (Inertial frames, stationary observers and the adopted Galilean transformations between frames clause (iv)), and let x~(t′,ρ):=Qx(t′−b,ρ)+u(t′−b)+a, τ~(t′):=Qτ(t′−b) be the transformed motion and datum of Adoption of the external-torque branch of the rigid-material model: declared torque data and the balance of angular momentum about the centre of mass clause (vii). Then the balance holds in the second frame, and Iω~′(t′)+ω~(t′)×Iω~(t′)=R~(t′)Tτ~(t′)(t′∈I0+b), where ω~(t′)=ω(t′−b) and R~(t′)=QR(t′−b); the body-frame torque is unchanged: R~(t′)Tτ~(t′)=R(t′−b)Tτ(t′−b).

The statement is conditional on the adopted model and torque balance; it asserts no force law for τ, no conservation of Lc and no measured value.

Facts & Assumptions

Given: The model data and motion of the statement, the balance hypothesis Lc′=τ of Adoption of the external-torque branch of the rigid-material model: declared torque data and the balance of angular momentum about the centre of mass clause (iii), and the derivative of the configuration path.

[L2]

The balance: Lc′(t)=τ(t) on I0, and τ is continuous (Adoption of the external-torque branch of the rigid-material model: declared torque data and the balance of angular momentum about the centre of mass clauses (ii) and (iii)).

[L3]

Matrix-curve calculus: for the C1 curves R:I0→SO(3) and l:I0→R3 one has (Rl)′=R′l+Rl′; RTR′=[ω]× and R′=R[ω]×; [ω]×z=ω×z; and RTR=I3, so RTw=0 implies w=0 (Derivative rules for differentiable matrix-valued curves, and skewness of RTR′ for a curve in SO(3), The skew-matrix/cross-product correspondence [ω]×z=ω×z and its conjugation law R[ω]×RT=[Rω]×, The orthogonal group O(3) and the rotation group SO(3), Rectangular matrix multiplication and the identity matrix In, including zero-sized shapes).

[L4]

Cross-product algebra: u×v is bilinear and alternating, u×u=0, u×v=−(v×u), and ⟨u,v×w⟩=det⁡[u v w], so a cross product is orthogonal to each factor (The cross product is bilinear, alternating, and orthogonal to both factors, The cross product in R3, The Euclidean inner product ⟨x,y⟩=∑k<nxkyk on Rn).

[L5]

Principal data: the positively oriented orthonormal eigenbasis (ej) and principal moments Ij of I, with Iω=∑jIjωjej when ω=∑jωjej (Principal axes and principal moments of the inertia data of a rigid-material model, axis moments and extremal values clauses (a)-(b)).

[L6]

Pairing derivative and constancy: for differentiable curves u,v the scalar product t↦⟨u(t),v(t)⟩ is differentiable with derivative ⟨u′,v⟩+⟨u,v′⟩ (Differentiation of sums, scalar multiples, inner products, cross products and squared norms of differentiable curves in R3 clause 2); a continuous real function on an interval whose derivative vanishes at every interior point is constant (A function continuous on an interval I whose derivative vanishes at every interior point of I is constant on I; consequently two such functions with the same derivative differ by a constant).

[L7]

Frame changes: the description of the motion in the second frame has configuration path (c~,R~) with R~(t′)=QR(t′−b), body angular velocity ω~(t′)=ω(t′−b), and inertial quantities L~c(t′)=QLc(t′−b) (Behaviour of the rigid-material configuration, angular velocity, inertia data and inertial quantities under a change of inertial frame clauses 1, 2 and 5); differentiation of a composition with the affine reparametrisation t↦t′−b and the constant rotation Q follows the chain rule (The chain rule for total derivatives: D(g∘f)(a)=Dg(f(a))∘Df(a)).

[L8]

Nondegeneracy: for a nondegenerate model the symmetric matrix I is positive definite and invertible (Principal axes and principal moments of the inertia data of a rigid-material model, axis moments and extremal values clause (d)); consequently I−1l=I−1Iω=ω for l=Iω, the inverse satisfying I−1I=I3 (Invertible matrices and the general linear group GL⁡n(F), Rectangular matrix multiplication and the identity matrix In, including zero-sized shapes).

Proof

technique · direct; differentiate $Rl$ with the product rule, translate the balance into the body frame, read off components in a principal basis, differentiate the quadratic form, and instantiate the frame-transformation laws
1.1givenL1L2L3algebra

By [L1] and [L3] the product Rl is differentiable on I0 with (Rl)′=R′l+Rl′=R([ω]×l+l′)=R(ω×l+l′), and by [L2] this equals τ. Multiplying by RT and using RTR=I3 gives ω×l+l′=RTτ.

1.2givenL2L7algebra

Let t′=t+b and use [L7]: ω~(t′)=ω(t′−b) and L~c(t′)=QLc(t′−b); differentiating the second identity in t′ by the chain rule [L7] gives L~c′(t′)=QLc′(t′−b)=Qτ(t′−b)=τ~(t′), so the adopted balance holds in the second frame.

2.1step 1.1givenL1algebra

Since l=Iω and I is a constant matrix, l′=Iω′; substituting l=Iω into step 1.1 gives Iω′+ω×Iω=RTτ, which is clause 1 (and the alternative form l′=RTτ−ω×Iω).

2.2step 1.1givenL4L8algebra

Assume τ≡0 and nondegeneracy. From step 1.1, l′=−ω×l=(Iω)×ω=l×(I−1l), the middle equality by antisymmetry [L4] and the last by I−1l=ω from [L8]; similarly ω′=I−1(−ω×Iω)=F(ω), which is clause 4.

3.1step 2.1givenL3L4L5algebra

In the positively oriented principal basis of [L5], the basis matrix Q belongs to SO(3) and the skew/cross correspondence [L3] gives Q(u×v)=(Qu)×(Qv), so the usual cross-product coordinates apply. Any orthonormal principal basis can be given this orientation by negating one eigenvector, without changing eigenvalues or the motion. Iω=∑jIjωjej and the first component of ω×Iω is ω2I3ω3−ω3I2ω2=(I3−I2)ω2ω3, with the cyclic analogues; writing RTτ=∑jτjej, clause 1 reads I1ω1′=(I2−I3)ω2ω3+τ1 and cyclically, which is clause 2.

3.2step 2.1givenL1L4L6algebra

Differentiating Krot=12⟨ω,Iω⟩ with [L6] and using the symmetry of I from [L1] gives Krot′=⟨ω′,Iω⟩=⟨ω,Iω′⟩; substituting Iω′=RTτ−ω×Iω from step 2.1 and using ⟨ω,ω×Iω⟩=0 by [L4] gives Krot′=⟨ω,RTτ⟩, which is clause 3; when τ≡0 this derivative vanishes identically and [L6] makes Krot constant on I0. The identification with the kinetic splitting is clause 3 of Total momentum, kinetic-energy splitting and centre-of-mass angular momentum of a rigid-material motion.

4.1step 1.2step 2.1givenL3L7algebra∎

Applying step 2.1 in the second frame (whose configuration path is (c~,R~) of class C2 by [L7]) gives Iω~′+ω~×Iω~=R~Tτ~ on I0+b; and R~(t′)Tτ~(t′)=R(t′−b)TQTQτ(t′−b)=R(t′−b)Tτ(t′−b) because QTQ=I3 [L3], so the body-frame torque is unchanged; this is clause 5.

Remarks

  • What is a theorem and what is an assumption. The balance Lc′=τ is adopted in Adoption of the external-torque branch of the rigid-material model: declared torque data and the balance of angular momentum about the centre of mass; clauses 1-4 here are its consequences in the body frame and in the torque-free case, and clause 5 records that the formulation is consistent with the framework's frame changes. No clause produces τ from a force system.

  • Where the nondegeneracy is used. Clauses 1-3 and 5 hold for every model of the branch, including degenerate ones; only clause 4 uses the invertibility of I, and the items that invert I on this page state that hypothesis explicitly.

  • The rotational power identity. Clause 3 says that the rate of change of the rotational kinetic energy equals the power ω⋅RTτ developed by the external torque; in the torque-free branch the rotational kinetic energy is a constant of the motion. This is a consequence of the adopted balance, not a separate assumption, and it does not by itself determine the motion.

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