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Reduction of the heavy symmetric top branch: pivotal angular momentum, Euler-angle equations, the two conserved momenta and the one-dimensional θ equation

Physical scope

Conditional deductions inside the heavy symmetric top branch of Adoption of the heavy symmetric top branch: axisymmetric rigid material, a fixed pivot material point, a uniform gravitational field and the balance of angular momentum about the pivot for the rigid-material model of Adoption of the rigid-material model branch: reference mass distribution, rigid placements, orientation and scope: the angular momentum about the pivot equals RI~ω with I~ the inertia about the pivot; the pivot balance gives the body-frame equations; and on any interval on which the orientation is described by the Euler-angle chart with θ∈(0,π) the motion satisfies the heavy-top system with parameters equal to the pivot transverse moment A=Ac+md2, the axial moment C=Cc, the total mass m, the pivot distance d and the field strength g, so the conserved momenta, the reduced energy and the one-dimensional θ equation hold. The statement carries the countable-choice assumption used only for the finiteness of the defining integrals, assumes the chart description as an explicit hypothesis, asserts nothing at the chart's poles, excludes friction and driving torques at the pivot, and asserts no measured value.

Statement

Assume the Axiom of Countable Choice ACω (The Axiom of Countable Choice (ACω)), used only for the finiteness of the defining integrals of the model's inertial quantities. Adopt the heavy symmetric top branch Adoption of the heavy symmetric top branch: axisymmetric rigid material, a fixed pivot material point, a uniform gravitational field and the balance of angular momentum about the pivot with parameters Ac>0, Cc>0, d>0, g>0 and total mass m>0; use the notation of that postulate: the pivot material point ρp=−d e3 is held at the origin, so c(t)=d R(t)e3; the pivot reaction contributes no torque about the origin; and the external gravitational field is G=−ge3 with total torque about the origin τp(t)=−mgd (R(t)e3)×e3. Put A:=Ac+md2>0,C:=Cc>0, the transverse moment of the model about the pivot and its axial moment. Let x(t,ρ)=c(t)+R(t)ρ be a motion of the branch with time window I0, and suppose that there are functions φ,θ,ψ:I0→R of class C2 with θ(I0)⊆(0,π) and R(t)=Θ(φ(t),θ(t),ψ(t))=Rz(φ(t))Ry(θ(t))Rz(ψ(t))(t∈I0), the Euler-angle description of The Euler-angle parametrization and the heavy symmetric top system. Then:

  1. Angular momentum about the pivot. With ω the body angular velocity of the motion and I~:=A (e1e1T+e2e2T)+C e3e3T (the diagonal matrix diag(A,A,C) in the principal basis) one has Jp(t):=∫x(t,ρ)×∂tx(t,ρ) dν(ρ)=R(t) I~ ω(t), and the balance of Adoption of the heavy symmetric top branch: axisymmetric rigid material, a fixed pivot material point, a uniform gravitational field and the balance of angular momentum about the pivot clause (v) reads Jp′=τp with τp(t)=−mgd (R(t)e3)×e3,τp(t)⋅e3=0.
  2. Body-frame pivot equations. With γ(t):=R(t)Te3, I~ ω′+ω×I~ ω=−mgd (e3×γ)on I0, that is, componentwise in the principal basis, Aω1′=(A−C)ω2ω3+mgd γ2,Aω2′=(C−A)ω1ω3−mgd γ1,Cω3′=0. Under the Euler-angle description of the statement, γ=(−sin⁡θcos⁡ψ, sin⁡θsin⁡ψ, cos⁡θ),ω3=ψ′+φ′cos⁡θ.
  3. Reduction to one dimension. Define on I0 b:=C(ψ′+φ′cos⁡θ),a:=A φ′sin⁡2θ+bcos⁡θ. Then b and a are constant on I0; consequently φ′=a−bcos⁡θAsin⁡2θ,ψ′=bC−(a−bcos⁡θ)cos⁡θAsin⁡2θ; the reduced energy E:=12A θ′2+(a−bcos⁡θ)22Asin⁡2θ+b22C+mgdcos⁡θ is constant on I0; and with the effective potential U(θ):=(a−bcos⁡θ)22Asin⁡2θ+b22C+mgdcos⁡θ one has A θ′′=−U′(θ) on I0.
  4. The heavy-top system. Equivalently, (φ,θ,ψ) is a heavy-top trajectory of The Euler-angle parametrization and the heavy symmetric top system with parameters (A,C,m,d,g), and clauses 1-4 of Reduction of the heavy symmetric top system: conserved momenta, one-dimensional θ equation and conserved reduced energy hold for it.

The statement assumes the Euler-angle description as a hypothesis on the interval: no claim is made that every motion of the branch admits such a description, that a description extends across the poles θ∈{0,π} (where the sleeping-top and hanging configurations lie), or that the description is unique. On every subinterval on which a description with θ∈(0,π) exists, the conclusions hold there. The statement asserts no friction or driving torque at the pivot, no measurement and no empirical value.

Facts & Assumptions

Given: The heavy-top branch data Ac,Cc,d,g,m, the derived constants A=Ac+md2 and C=Cc, a motion x(t,ρ)=c(t)+R(t)ρ of the branch with time window I0, and a C2 Euler-angle description (φ,θ,ψ) of R with θ(I0)⊆(0,π).

[L1]

Branch kinematics: the pivot material point ρp=−de3 satisfies c(t)+R(t)ρp=0, so c(t)=d R(t)e3; the pivot reaction contributes no torque about the origin; the gravitational torque about the origin is τp=mc×(−ge3); and the adopted balance is Jp′=τp with Jp=∫x×∂tx dν (Adoption of the heavy symmetric top branch: axisymmetric rigid material, a fixed pivot material point, a uniform gravitational field and the balance of angular momentum about the pivot clauses (iii)-(v), Configuration, configuration space and orientation of a rigid-material model in an inertial frame, Body and spatial angular velocity of a rigid-material motion, and the material velocity field).

[L2]

Inertial identities of the model: P:=∫∂tx dν=mc′, Lc:=∫(x−c)×(∂tx−c′) dν=RIω, and for Jp=∫x×∂tx dν one has Jp=Lc+c×P (Total momentum, kinetic-energy splitting and centre-of-mass angular momentum of a rigid-material motion clauses 2 and 4, The Lebesgue integral is linear on L1(μ), Finiteness of the moments of a bounded finite Borel measure on R3, Mass distributions on R3: total mass, first moment and inertia matrix).

[L4]

Euler-angle kinematics: for R=Θ(φ,θ,ψ) with θ∈(0,π) the body angular velocity is ω=(−φ′sin⁡θcos⁡ψ+θ′sin⁡ψ, φ′sin⁡θsin⁡ψ+θ′cos⁡ψ, ψ′+φ′cos⁡θ) in the standard basis, and ω12+ω22=θ′2+φ′2sin⁡2θ (Angular velocity in Euler angles: ω3=ψ′+φ′cos⁡θ and ω12+ω22=θ′2+φ′2sin⁡2θ); the coordinate rotation matrices satisfy Ry(a)e3=sin⁡a e1+cos⁡a e3 and Rz(b)Te1=cos⁡b e1−sin⁡b e2, Rz(b)Te3=e3 (The coordinate rotation matrices Rz(a) and Ry(a): values in SO(3), composition law, and derivatives); and sin⁡2+cos⁡2=1 (Sine and cosine defined by their real power series, The derivatives of sine and cosine are cosine and minus sine).

[L5]

The heavy-top system: The Euler-angle parametrization and the heavy symmetric top system defines a heavy-top trajectory by the three displayed equations ddt(Aφ′sin⁡2θ+Ccos⁡θ(ψ′+φ′cos⁡θ))=0, ddt(Aθ′)=Aφ′2sin⁡θcos⁡θ−C(ψ′+φ′cos⁡θ)φ′sin⁡θ+mgdsin⁡θ and ddt(C(ψ′+φ′cos⁡θ))=0, and Reduction of the heavy symmetric top system: conserved momenta, one-dimensional θ equation and conserved reduced energy derives from them the conservation of b and a, the formulas for φ′ and ψ′, the constant reduced energy E and the equation Aθ′′=−U′(θ) with the displayed U (Reduction of the heavy symmetric top system: conserved momenta, one-dimensional θ equation and conserved reduced energy clauses 1-4).

[L6]

Calculus and algebra: (Rl)′=R′l+Rl′, R′=R[ω]× and [ω]×z=ω×z for a C1 rotation path (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)); the cross product is bilinear and alternating with u×(u×w)=(u⋅w)u−∥u∥22w for unit u (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); the chain, product and quotient rules hold for the scalar functions below (The chain rule for total derivatives: D(g∘f)(a)=Dg(f(a))∘Df(a), Sums, scalar multiples, products and quotients: (f+g)′(c)=f′(c)+g′(c), (αf)′(c)=αf′(c), (fg)′(c)=f′(c)g(c)+f(c)g′(c), and (f/g)′(c)=(f′(c)g(c)−f(c)g′(c))/g(c)2 when g(c)≠0, The derivative f′(c)=lim⁡x→cf(x)−f(c)x−c of f:A→R at a point c∈A that is a limit point of A, and differentiability on a set, Intervals of R: the nine order-convex forms, nondegeneracy, and length); and a continuous real function on an interval with vanishing derivative 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).

Proof

technique · direct; compute the pivotal angular momentum from the model's inertial identities, translate the adopted balance into the body frame, and read the resulting equations in the Euler-angle chart, then invoke the supplier's reduction
1.1givenL1L6

By [L1] the constraint gives c(t)=dR(t)e3, and since R is C1 with R′=R[ω]× by [L6] one has c′=dR′e3=dR[ω]×e3=dR(ω×e3).

1.2givenL4algebra

By [L4], reading the columns of the three factors and using θ(I0)⊆(0,π), the vector γ=RTe3=Rz(ψ)TRy(θ)TRz(φ)Te3=Rz(−ψ)Ry(−θ)e3 equals Rz(−ψ)(−sin⁡θ e1+cos⁡θ e3)=(−sin⁡θcos⁡ψ, sin⁡θsin⁡ψ, cos⁡θ), and ω3=ψ′+φ′cos⁡θ.

2.1step 1.1givenL1L6

By [L1] the gravitational force system of the branch acts as the total force −mge3 applied at the centre of mass, whose torque about the origin is τp=mc×(−ge3); with c=dRe3 from step 1.1 this is τp=−mgd(Re3)×e3, and τp⋅e3=0 because the cross product is orthogonal to its factors by [L6].

3.1step 1.1step 2.1givenL1L2L3L6algebra

By [L2] one has Jp=Lc+c×P=RIω+mc×c′. Substituting c=dRe3 and c′=dR(ω×e3) from step 1.1 and using Ie3=Ce3, Ie1=Ace1, Ie2=Ace2 from [L3] gives mc×c′=md2 (Re3)×R(ω×e3)=md2R(e3×(ω×e3))=md2R(ω−ω3e3) by [L6] and the vector triple product with ∥e3∥2=1, so Jp=R(Iω+md2(ω−ω3e3))=RI~ω with I~=diag(A,A,C) and A=Ac+md2, C=Cc. Hence the balance of [L1] reads Jp′=τp with τp as in step 2.1, completing clause 1.

4.1step 1.2step 2.1step 3.1givenL6algebra

Since R is C1 and ω is C1, the product I~ω is C1 and Jp=RI~ω from step 3.1 gives R(I~ω′+ω×I~ω)=Jp′ by [L6]; with the balance Jp′=τp of step 3.1 and RTR=I3 one gets I~ω′+ω×I~ω=RTτp. By step 2.1 and [L6], RT((Re3)×e3)=e3×(RTe3)=e3×γ with γ of step 1.2, so I~ω′+ω×I~ω=−mgd(e3×γ). Componentwise, (e3×γ)1=−γ2, (e3×γ)2=γ1, (e3×γ)3=0 and (ω×I~ω)1=(C−A)ω2ω3, (ω×I~ω)2=(A−C)ω1ω3, (ω×I~ω)3=0, giving the three displayed equations of clause 2.

5.1step 1.2step 4.1givenL6

The third of the equations of step 4.1 gives Cω3′=0, and C>0, so ω3 is constant on the interval I0 by [L6]; by step 1.2, b=C(ψ′+φ′cos⁡θ)=Cω3 is constant on I0.

6.1step 1.2step 2.1step 3.1step 5.1givenL4L6algebra

By step 3.1 and [L6], ddt(Jp⋅e3)=Jp′⋅e3=τp⋅e3=0 by step 2.1, so Jp⋅e3 is constant on I0; and by steps 3.1 and 1.2, Jp⋅e3=(RI~ω)⋅e3=I~ω⋅γ=A(ω1γ1+ω2γ2)+Cω3γ3. Substituting the components of [L4] and step 1.2 and using sin⁡2ψ+cos⁡2ψ=1 from [L4] gives ω1γ1+ω2γ2=φ′sin⁡2θ and ω3γ3=(ψ′+φ′cos⁡θ)cos⁡θ, so Jp⋅e3=Aφ′sin⁡2θ+bcos⁡θ=a is constant on I0.

6.2step 1.2step 4.1step 5.1givenL4L6algebra

Put n:=sin⁡ψ e1+cos⁡ψ e2, so that n has ∥n∥2=1 and, by [L4] and R′=R[ω]×, the identity θ′=ω⋅n holds. Differentiating θ′ with [L6] gives Aθ′′=A(ω′⋅n)+A(ω⋅n′), where n′=ψ′(cos⁡ψ e1−sin⁡ψ e2); using the first two equations of step 4.1, the components of [L4] and the values ω1cos⁡ψ−ω2sin⁡ψ=−φ′sin⁡θ, ω2sin⁡ψ−ω1cos⁡ψ=φ′sin⁡θ and γ2sin⁡ψ−γ1cos⁡ψ=sin⁡θ of step 1.2, one computes A(ω′⋅n)=(A−C)ω3 φ′sin⁡θ+mgd sin⁡θ and A(ω⋅n′)=−Aφ′ψ′sin⁡θ, hence Aθ′′=(A−C)ω3φ′sin⁡θ+mgdsin⁡θ−Aφ′ψ′sin⁡θ=Aφ′2sin⁡θcos⁡θ−bφ′sin⁡θ+mgdsin⁡θ, the last equality by ω3−ψ′=φ′cos⁡θ from step 1.2 and b=Cω3 from step 5.1.

7.1step 5.1step 6.1step 6.2givenL5∎

The three equations of the definition of [L5] hold: the first is ddt(Aφ′sin⁡2θ+Ccos⁡θ(ψ′+φ′cos⁡θ))=a′=0 by step 6.1, the third is ddt(C(ψ′+φ′cos⁡θ))=b′=0 by step 5.1, and the second is Aθ′′=Aφ′2sin⁡θcos⁡θ−C(ψ′+φ′cos⁡θ)φ′sin⁡θ+mgdsin⁡θ by step 6.2 with C(ψ′+φ′cos⁡θ)=b. Therefore (φ,θ,ψ) is a heavy-top trajectory of [L5] with parameters (A,C,m,d,g), and clauses 1-4 of Reduction of the heavy symmetric top system: conserved momenta, one-dimensional θ equation and conserved reduced energy apply: a and b are constant, φ′ and ψ′ are given by the displayed formulas, the reduced energy E is constant, and Aθ′′=−U′(θ). This proves clauses 3 and 4.

Remarks

  • Where A=Ac+md2 comes from. The transverse moment of the model about the pivot is the transverse moment Ac about the centre of mass shifted by md2; this is why the reduction uses A and the supplier's parameter is identified with the pivot moment, not with Ac. The axial moment is unchanged because the shift is along the symmetry axis.

  • The role of the chart. The Euler-angle description is a hypothesis; the chart is singular at the poles θ=0,π, where the sleeping top and the hanging configuration lie, and the statement says nothing there. The definitions of a, b, E and U depend on the chosen description (the angles are determined only up to the chart's ambiguities), while the physical conclusions of clause 3 are invariants of the motion.

  • No empirical content. Clause 3 is a conditional deduction from the adopted branch; in particular the sleeping-top threshold, the stability of the upright top and the interpretation of precession in any concrete apparatus are not asserted here, and no value of Ac, Cc, m, d or g is measured.

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