The rotating-frame effective potential of the circular restricted three-body problem has negative singular wells at both primaries. Its three Collinear Lagrange points are planar saddles, and its two Triangular Lagrange points are planar local maxima for nonzero primary masses. These geometric labels do not replace a dynamical stability analysis including the Coriolis force.
Past exam of the mathematics course of the University of Cambridge 2012 iii Paper 59 4 Solution Created 2026-10-03 Updated 2026-10-07
Let and , with . In the centre of mass frame the two primary distances are and . Applying Newton's law of universal gravitation and circular centripetal acceleration to the first primary gives , and henceThe same result follows from the second primary or from the relative two-body equation of motion.
A rotating-frame equilibrium has zero rotating-frame velocity, so its Coriolis force vanishes. Above the orbital plane both primaries have downward gravitational components; below it both have upward components. The centrifugal force has no component. More explicitly,which vanishes only at for finite nonsingular points. Thus all equilibria lie in the orbital plane.
The equation of motion in a rotating frame for the dwarf isOn the orbital plane the centrifugal contribution is . Thus the rotating-frame effective potential is ; equilibria are exactly its stationary points. The Coriolis force affects motion about those equilibria but not their positions. This is the circular restricted three-body problem, with the dwarf treated as a test mass.
The printed energy unit has the wrong dimensions. The correct total energy unit is , or for specific energy; is an acceleration. Dividing by and measuring lengths in units of gives the dimensionless effective potentialThe primary coordinates are and . Restricting to gives andThe absolute values are essential; dropping them would reverse the attraction on the left of a primary. On each of the intervals separated by the two primaries, decreases strictly from to . There is exactly one Collinear Lagrange point on each interval, a maximum along the direction.
For the inner Lagrange point, write with . For the L2 Lagrange point, write . The respective equations areBalancing the leading terms gives . Therefore the small-mass-ratio collinear Lagrange points obeyThe omitted displacement of the secondary is smaller than the stated error. The leading distance from the secondary is the dimensionless Hill radius.
For the L3 Lagrange point put . It lies to the left of both primaries, soExpanding the two positive inverse-square factors gives and . Thus , soAll three have . The small- equalities in the paper are asymptotic expressions, not exact coordinates for finite mass ratio.
For the remaining Lagrange points, introduce plane polar coordinates about the first primary: , . Its distance to the second primary is , andThe angular stationary condition is . For an off-axis point and , so . The radial stationary condition becomesHence , and implies . The Triangular Lagrange points are exactlyBoth triangles are equilateral. The collinear and off-axis calculations together exhaust the stationary points.
For the requested sketch, tends to at either primary and at large in-plane radius. Each Collinear Lagrange point is a saddle of the planar effective potential: its curvature is negative and its curvature is positive. To see the latter, let , and . At an inner point both distances are below one, so . At an exterior stationary point, use barycentric positions , and weights : the equation implies . To the right, the weighted sum is positive because the positive primary is closer; to the left it is negative because the negative primary is closer. Thus there as well, and .
At either Triangular Lagrange point, the planar Hessian isIts trace is and determinant , so these are local maxima. Their height is . The sketch below uses a finite mass ratio to separate the five points clearly; its singular wells are clipped only for display. These curvature labels concern the effective potential, not a stability test that ignores the Coriolis force.
Rotating binary effective-potential surface and contours at mass fraction 0.10, with all five Lagrange points marked
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