I was revisiting triple integrals, so I decided to give this a go. This is the result:
As expected, the pole wins.
Development
Starting from Newton's law of universal gravitation: $$\mathrm d\mathbf g = G\frac{\mathbf r\ \mathrm dm}{\left|\mathbf r\right|^3}$$
And the parametrization of our oblate asteroid: $$(x,y,z) = \mathbf r(r,\theta,\phi)=\left[\alpha\cdot(r\sin\phi\cos\theta+1),\beta\cdot r\sin\phi\sin\theta,\gamma\cdot r\cos\phi\right]$$
This leaves the origin exactly on the equator or pole, depending on the choices of the semi-major axis lengths $\alpha$, $\beta$ and $\gamma$:
- $\alpha=\beta>\gamma$ leaves us at the equator.
- $\alpha<\beta=\gamma$ leaves us at the pole.
Note that the asteroid's centroid is in the x-axis:
(this with radii 0.7, 1.0, 1.0):
Change of variables gives: $$g_x=G\alpha\beta\gamma\rho\int_0^1\int_0^{2\pi}\int_0^\pi\frac{xr^2\sin\phi}{\left(x^2+y^2+z^2\right)^\frac{3}{2}}\mathrm d\phi\ \mathrm d\theta\ \mathrm dr$$
Note I left cartesian variables there, because I was going to do this numerically. Also, naturally $g_y=g_z=0$. Also, $\rho$ is density (I used it to test Earth).
I fired up Scilab and learned the int3d
function. Results with Earth were fine, so I decided it was good enough for the plot above. For completeness, Earth data used was:
Equator radius: 6,378,136.6 m
Pole radius: 6,356,751.9 m (source)
Density: 5,520 kg/m³ // (source)
Gravitational constant: 6.67384e-11
Gravity on equator: 9.8289 m/s²
Gravity on pole: 9.8354 m/s²
I think this is good, considering on equator there's ~0.3% less gravity due to Earth's rotation, which yields closer to our usual 9.8 m/s². Also, Earth's almost a sphere, and the results were realistically close to each other I guess.