Partial Differential Equations - Modelling and ... - ResearchGate
Partial Differential Equations - Modelling and ... - ResearchGate
Partial Differential Equations - Modelling and ... - ResearchGate
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Reduced-Order <strong>Modelling</strong> of Dispersion 251<br />
value for a white noise for angles between 0 <strong>and</strong> π. Onced is calculated by this<br />
procedure one needs to define d ⊥ E which is unknown as B⊥ is unknown. We<br />
make the approximation d ⊥ E ∼ d E(B,B ∗ )whereB ∗ is the projection of B over<br />
the vector u, the averaged velocity along the polynomial characteristic. This<br />
approach gives satisfactory results for smooth atmospheric flow fields which<br />
is our domain of interest as no phyto treatments is, in principle, applied when<br />
the wind is too strong or if the temperature is too high (e.g., for winds stronger<br />
than 20 km/h <strong>and</strong> air temperature more than 30 ◦ C). This also makes that the<br />
polynomial construction above gives satisfaction with low order polynomials.<br />
Ground Variations<br />
At this point one accounts for the topography or ground variations ((x, y) →<br />
ψ(x, y)) in the prediction model above. These are available from digital terrain<br />
models (DTM) [Arc06]. Despite this plays an important role in the dispersion<br />
process, it is obviously hopeless to target direct simulation based on a detailed<br />
ground description. One should mention that ground variations effects are implicitly<br />
present in observation data for wind <strong>and</strong> transport as mentioned in<br />
Section 2.2. However, as we said, observations are quite incomplete <strong>and</strong> to<br />
improve the predictive capacity of the model one needs to model the dependency<br />
between ground variations <strong>and</strong> migration time. Therefore, in addition<br />
to the mentioned assimilation problem, one scales the migration times used<br />
for transport over large distances by a positive monotonic decreasing function<br />
f(φ) with f(0) = 1 where<br />
φ =(∇ x,y ψ · u H )/‖u H ‖.<br />
Here u H is the ‘close to ground’ constructed flow field based on the assimilated<br />
observations.<br />
3 Parameter <strong>and</strong> Source Identification<br />
Two types of inverse problems have been treated. The first inverse problem<br />
is for parameter identification in the model above assimilating either local<br />
experimental data (as described in Section 2.1) or partial data available on<br />
wind u obs <strong>and</strong> transported species c obs measured by localized apparatus. In<br />
particular, the unknown parameters in our global transport model comes from<br />
the solution of a minimization problem for:<br />
J(p, u obs ,c obs )=‖c(p, u(p, u obs )) − c obs ‖, (6)<br />
where p gathers all unknown independent parameters in Section 2.2. ‖·‖ is<br />
a discrete L 2 -norm over the measurement points. u(p) is the completion of<br />
available wind measurements (u obs ) over the domain described in Section 2.2.