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lidar points directly at the sun the spectral power density is insufficient to cause a problem,<br />
and the interaction between two adjacent lidars can be neglected. Thorough electromagnetic<br />
screening eliminates the risk of spurious spectral features caused by electrical interference for<br />
any normal deployment.<br />
4.3.5 Time-of-flight considerations<br />
The round-trip time for light interrogating the atmosphere at a height of 100 m is less than 1<br />
µs. On this timescale the ZephIR scanner moves the focused beam a distance of only 300 µm,<br />
and thelaserphasedrifts byan insignificantamount.Thepolarisationstate ofthelidaroutput<br />
is similarly frozen on this timescale, so no appreciable misalignment of loss of interference<br />
efficiency is incurred.<br />
4.4 End-to-end measurement process for CW Doppler lidar<br />
4.4.1 Introduction<br />
The wind parameter measurement process can be divided into a number of sequential steps.<br />
This section describes the overall end-to-end process of the wind speed measurement process<br />
for a CW coherent Doppler lidar wind profiler. Again, where appropriate, the ZephIR lidar is<br />
used as an example.<br />
4.4.2 Transmitter optics<br />
The role of the transmitter is to provide a focused beam at a desired location. This location<br />
can be moved around in space with a combination of (i) altering the focus range and (ii)<br />
passingthebeamthroughascanningelementsuchasarotatingprism(wedge).Windprofiling<br />
lidars conveniently employ a conical scan with its axis aligned vertically; the cone half-angle is<br />
commonly of order 30 ◦ (i.e. the beam elevation angle is ∼ 60 ◦ ). Some turbine mounted lidars<br />
use lower cone angles, the optimum choice depending upon a variety of factors including the<br />
mounting position on the turbine, the rotor diameter and the measurement ranges of most<br />
interest.<br />
In a monostatic CW system, a Doppler-shifted contribution to the signal is generated via<br />
light scattering from any moving part of the atmosphere that the beam illuminates. The<br />
contribution from any point is weighted by the square of the beam’s intensity at that point<br />
(Harris et al., 2001a). Hence it can be shown that focusing of an ideal Gaussian beam<br />
(Siegman, 1986) gives rise to a spatial sensitivity along the beam direction that depends on<br />
the inverse of beam area. It follows that the sensitivity rises to a peak at the beam waist, and<br />
falls symmetrically on either side. There is also a spatial dependence of sensitivity transverse<br />
to the beam, but because the beam is very narrow this is of little interest and can be ignored.<br />
To a good approximation the axial weighting function for a CW monostatic coherent lidar is<br />
given by a Lorentzian function (Sonnenschein and Horrigan, 1971; Karlsson et al., 2000):<br />
F = Γ/π<br />
∆ 2 +Γ 2,<br />
where ∆ is the distance from the focus position along the beam direction, and Γ is the halfwidth<br />
of the weighting function to the -3 dB point, i.e. 50% of peak sensitivity. Note that<br />
F has been normalised such that it’s integral from −∞ to ∞ gives unity. To another good<br />
approximation, Γ is given by:<br />
Γ = λR2<br />
πA2, (92)<br />
where λ is the laser wavelength, here assumed to be the telecommunications wavelength<br />
λ ∼ 1.55×10 −6 m, R is the distance of the beam focus from the lidar output lens, and A is<br />
78 <strong>DTU</strong> Wind Energy-E-Report-0029(EN)<br />
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