Research Article
The Effect of Rigging Angle on Longitudinal Direction Motion of Parafoil-Type Vehicle: Basic Stability Analysis and Wind Tunnel Test
Table 9
Wind tunnel test result of 100 Pa wind condition.
| Data number | Rigging angle RA [deg] | Uncertainty of RA | Angle of attack α [deg] | Uncertainty of α | Angle of attitude θ [deg] | Uncertainty of θ |
| 1 | -6.0 | 0.24 | 1.742 | 0.599 | -4.258 | 0.647 | 2 | -6.0 | 0.24 | 1.372 | 0.612 | -4.628 | 0.659 | 3 | -5.0 | 0.24 | 3.136 | 0.605 | -1.864 | 0.652 | 4 | -5.0 | 0.24 | 2.898 | 0.601 | -2.102 | 0.649 | 5 | -4.0 | 0.24 | 4.534 | 0.621 | 0.534 | 0.667 | 6 | -4.0 | 0.24 | 4.509 | 0.636 | 0.509 | 0.681 | 7 | -3.0 | 0.24 | 6.157 | 0.660 | 3.157 | 0.703 | 8 | -3.0 | 0.24 | 6.320 | 0.681 | 3.320 | 0.723 | 9 | -2.0 | 0.24 | 8.100 | 0.723 | 6.100 | 0.763 | 10 | -2.0 | 0.24 | 7.920 | 0.777 | 5.920 | 0.814 | 11 | -1.0 | 0.24 | 9.500 | 0.746 | 8.500 | 0.784 | 12 | -1.0 | 0.24 | 9.350 | 0.768 | 8.350 | 0.805 | 13 | 0.0 | 0.24 | 11.00 | 0.802 | 11.00 | 0.838 | 14 | 1.0 | 0.24 | 13.03 | 0.801 | 14.03 | 0.837 | 15 | 1.0 | 0.24 | 13.22 | 0.815 | 14.22 | 0.850 | 16 | 2.0 | 0.24 | 14.63 | 0.853 | 16.63 | 0.887 |
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