Step 1: Formula and geometry.
The Eötvös correction accounts for the effect of ship motion on measured gravity:
\[
\Delta g_E = 2\,\omega\,V \cos\phi\,\sin\alpha \;+\; \frac{V^{2}}{R}\quad \text{(in m/s$^{2}$)},
\]
where \(\omega\) is Earth's angular speed, \(R\) is Earth's mean radius, \(\phi\) is latitude, and \(\alpha\) is the heading measured clockwise from North.
Here, \(\phi=\theta_1\) and \(\alpha=\theta_2\). The term with \(\sin\alpha\) gives the eastward component of velocity; the latitude factor is \(\cos\phi\).
Step 2: Convert to mGal and express in given speed units.
Use \(\omega = 7.292115\times10^{-5}\,\text{s}^{-1}\), \(R \approx 6.371\times10^{6}\,\text{m}\), and \(1\,\text{mGal}=10^{-5}\,\text{m/s}^2\).
\underline{If \(V\) is in km/h}: \(1\,\text{km/h}=0.27778\,\text{m/s}\).
Coefficient of the linear term:
\[
\frac{2\omega(0.27778)\times 10^{5}}{1} \approx 4.040.
\]
Coefficient of the quadratic term:
\[
\frac{(0.27778)^{2}}{R}\times 10^{5} \approx 0.001211.
\]
Hence,
\[
\Delta g_E(\text{mGal}) = 4.040\,V_1\cos\theta_1\sin\theta_2 + 0.001211\,V_1^{2}.
\]
This matches option (A).
\underline{If \(V\) is in knots}: \(1\,\text{knot}=0.51444\,\text{m/s}\).
Linear coefficient:
\[
2\omega(0.51444)\times10^{5}\approx 7.503.
\]
Quadratic coefficient:
\[
\frac{(0.51444)^{2}}{R}\times10^{5}\approx 0.004154.
\]
Hence,
\[
\Delta g_E(\text{mGal}) = 7.503\,V_2\cos\theta_1\sin\theta_2 + 0.004154\,V_2^{2},
\]
which is option (B).
Step 3: Eliminate the incorrect options.
(C) mixes units (uses \(V_2\) with km/h coefficients) and swaps \(\cos\theta_1\) and \(\sin\theta_2\).
(D) mixes units (uses \(V_1\) with knot coefficients).
Therefore, only (A) and (B) are correct.
\[
\boxed{\text{Correct options: (A) and (B)}}
\]