Figure 1.

Figure 2.

Figure 3.

Figure 4.

Figure 5.

Figure 6.

Figure 7.

Figure 8.

Results of the computational comparison between the different configurations at the two load points
| load point
| load point
| ||||
| Difference vector
| Δx [cm]: | 3.21 | 1.39 | ||
| Δy [cm]: | 0.52 | 1.84 | |||
| Δz: [cm]: | 3.60 | 3.57 | |||
| Euclidian norm
| 4.85 | 4.25 | |||
| Directional angle αi [°]: | 0.1 | 0.4 | |||
| initial configuration | end configuration | initial configuration | end configuration | ||
| elevation to the horizontal plane βi [°]: | 40.43 | 39.69 | 27.41 | 26.79 | |