Like kinetic energy, the angular momentum of a system of several bodies also decomposes into a “CM” contribution and an “internal” one.

Law — König's theorem for angular momentum

Ltot=rCM×ptotLCM+iri×miviLint\ev{\vec{L}_{\text{tot}} = \underbrace{\vec{r}_{\text{CM}}\times\vec{p}_{\text{tot}}}_{\vec{L}_{\text{CM}}} + \underbrace{\sum_i \vec{r}_i'\times m_i\vec{v}_i'}_{\vec{L}_{\text{int}}}} where ri=rirCM\vec{r}_i' = \vec{r}_i - \vec{r}_\text{CM} and vi=vivCM\vec{v}_i' = \vec{v}_i - \vec{v}_\text{CM} are the position and velocity of each body relative to the CM.

The two parts have distinct interpretations. LCM\vec{L}_\text{CM} (the orbital angular momentum): geometrically it is the angular momentum of a fictitious point mass placed at rCM\vec{r}_\text{CM} carrying the whole mass MtotM_\text{tot} and the whole momentum ptot\vec{p}_\text{tot}; practically, if the system is not rotating about its own CM, the whole of Ltot\vec{L}_\text{tot} reduces to LCM\vec{L}_\text{CM}.

Lint\vec{L}_\text{int} (the spin angular momentum): geometrically it is “how the system’s internal parts rotate” about the CM — think of a yo-yo in flight, whose Lint\vec{L}_\text{int} is the yo-yo’s spin. For a rigid body rotating with angular velocity ω\vec{\omega} about its own CM, Lint=ICMω\vec{L}_\text{int} = I_\text{CM}\,\vec{\omega}, where ICMI_\text{CM} is the moment of inertia about the CM.

If the total moment of the external forces is zero, the total angular momentum is conserved:

Mext=0    Ltot=constant\sum\vec{M}_{\text{ext}} = \vec{0} \;\Rightarrow\; \vec{L}_{\text{tot}} = \text{constant}

Context — Earth's dual angular momentum

The Earth possesses both an orbital angular momentum (LCM\vec{L}_\text{CM}: motion around the Sun) and a spin angular momentum (Lint\vec{L}_\text{int}: rotation about its own axis). Both are conserved, which explains why the Earth keeps rotating: no significant external force applies a braking moment.

Example — Two balls in motion

m1=4  kgm_1 = 4\;\text{kg} at r1=(1,1)\vec{r}_1 = (-1, 1) with v1=(0,3)  m/s\vec{v}_1 = (0, 3)\;\text{m/s}; m2=5  kgm_2 = 5\;\text{kg} at r2=(2,2)\vec{r}_2 = (2, -2) with v2=(6cos45,6sin45)=(4,24;  4,24)\vec{v}_2 = (6\cos 45^\circ, -6\sin 45^\circ) = (4{,}24;\; -4{,}24).

Centre of mass: rCM=4(1,1)+5(2,2)9=(6,6)9=(0,67;  0,67)\vec{r}_\text{CM} = \frac{4(-1,1) + 5(2,-2)}{9} = \frac{(6,\, -6)}{9} = (0{,}67;\; -0{,}67) vCM=4(0,3)+5(4,24;4,24)9=(21,2;  9,2)9=(2,35;  1,02)\vec{v}_\text{CM} = \frac{4(0,3) + 5(4{,}24;\,-4{,}24)}{9} = \frac{(21{,}2;\; -9{,}2)}{9} = (2{,}35;\; -1{,}02)

LCM\vec{L}_\text{CM} about the origin (ptot=MtotvCM=(21,2;9,2)\vec{p}_\text{tot} = M_\text{tot}\vec{v}_\text{CM} = (21{,}2;\, -9{,}2)): LCM=xCMpyyCMpx=0,67(9,2)(0,67)21,2=6,16+14,2=8,04L_\text{CM} = x_\text{CM}\,p_y - y_\text{CM}\,p_x = 0{,}67\cdot(-9{,}2) - (-0{,}67)\cdot 21{,}2 = -6{,}16 + 14{,}2 = 8{,}04

Lint\vec{L}_\text{int}: from the relative velocities v1=(0,3)(2,35;1,02)=(2,35;4,02)\vec{v}_1' = (0,3) - (2{,}35;\,-1{,}02) = (-2{,}35;\, 4{,}02) and v2=(4,24;4,24)(2,35;1,02)=(1,89;3,22)\vec{v}_2' = (4{,}24;\,-4{,}24) - (2{,}35;\,-1{,}02) = (1{,}89;\, -3{,}22), and from the relative positions, you compute the cross products ri×mivi\vec{r}_i'\times m_i\vec{v}_i' and sum them.

The centre of mass and angular momentum are the tools that let us pass from point-mass mechanics to the mechanics of rigid bodies and rotating systems, the subject of the next chapter.

Topics: Centre of mass Concepts: Angular momentum · Conservation of angular momentum · Moment of inertia Skills: Choice of pole

Related exercises: The rotating diver · Problem — Angular momentum of the Earth’s own rotation · Problem — Ranking ω for equal angular momentum