these areas, as shown inFigure 6. The simulation scenario consists of seven cells on the ground covering the areas around the flight trajectory. Each cell has three directional antennas, downtilted 120 degrees, with one main lobe (facing the ground) and two sidelobes (facing the sky). The ...
However, the same value for 𝐾𝑐𝑜𝑟𝑟Kcorr would lead to a suboptimal discharging trajectory for a vehicle mass of 32,000 kg (see Ib in Figure 15). Here, the SOC would still be at a value of 0.5 before the next recuperation phase where the battery is fully charged. This ...