Diurnal and planetary aberration

The rotation of the Earth on its axis produces aberration in an amount large enough to be taken into account in precise observational work.
Let an observer be at a place of latitude ∅ and let R_⊕, c and T be the Earth’s radius, the velocity of light and the number of seconds in one sidereal day. Then the observer O has velocity v due to the Earth’s rotation, given by

as easily seen by figure 1.

Figure 1. The velocity of an observer due to the rotation of the Earth.

Figure 2. The effect of diurnal aberration.
The constant of diurnal aberration κ₁ is then given in seconds of arc by

Evaluating, it is found that
κ₁ = 0''·32 cos ∅. (1)
Let us consider an observation made of a star of declination δ when it crosses the meridian. As the observer moves in an easterly direction due to the Earth’s rotation, diurnal aberration will cause the star to be seen east of its geocentric position. The star’s observed time of transit is, therefore, late by an amount Δt, obtained in the following way.
The star’s position at apparent transit is X₁ (figure 2) but its true position is X, where
XX₁ ≈ 0''·32 cos ∅.
Now if XX₁ is an arc of the star’s parallel of declination,
XX₁ = UV cos δ.
But UV is the delay in transit time since it is the difference in the hour angles of X and X₁. Hence, the delay time Δt is given by
Δt = UV = XX₁ sec δ = 0''·32 cosφ sec δ
that is
Δt = 0·^s021 cos∅ sec δ.
The declinations at transit, and, therefore, the meridian zenith distances, of the stars are not affected by diurnal aberration.
In the case of planets, the light entering the terrestrial observer’s eye comes from the direction the planet occupied at the epoch t₀ at which the light left the planet. In addition to the normal correction for stellar and diurnal aberration, therefore, a further correction is required to obtain the planet’s direction at the epoch t₁ at which it is observed. The time interval (t₁−t₀) is obtained from the planet’s geocentric distance divided by the velocity of light. If dα/dt and dδ/dt are the rates of change in geocentric right ascension and declination of the planet then the required corrections due to planetary aberration are given by (t₁ − t₀) dα/dt and (t₁ − t₀) dδ/dt.
It may also be mentioned in passing that in the case of an artificial Earth satellite with an orbital velocity of order 7 km s⁻¹, the aberration in its observed position is of order 5 arc sec and must be allowed for in precise tracking.