P = μ sin θ sin φ, Q = μ sin θ cos φ, R = φ + μ cos θ.
(4)
With CXF a quadrant, the components of angular velocity and momentum about OF, OY, are
P cos γ − R sin γ, Q, and A (P cos γ − R sin γ), AQ,
(5)
so that, denoting the components of angular momentum of the fly-wheel about OC, OX, OY, OZ by K or G′, h1, h2, h3,
h1 = A (P cos γ − R sin γ) cos γ + K sin γ,
(6)
h2 = AQ,
(7)