Research Article
The Effect of Rigging Angle on Longitudinal Direction Motion of Parafoil-Type Vehicle: Basic Stability Analysis and Wind Tunnel Test
Table 10
Wind tunnel test result of 120 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 | -7.0 | 0.24 | 0.525 | 0.600 | -6.475 | 0.648 | 2 | -6.0 | 0.24 | 1.298 | 0.614 | -4.702 | 0.661 | 3 | -6.0 | 0.24 | 1.451 | 0.637 | -4.549 | 0.683 | 4 | -5.0 | 0.24 | 2.404 | 0.609 | -2.596 | 0.656 | 5 | -5.0 | 0.24 | 2.766 | 0.619 | -2.234 | 0.666 | 6 | -4.0 | 0.24 | 4.142 | 0.644 | 0.142 | 0.688 | 7 | -3.0 | 0.24 | 6.416 | 0.742 | 3.416 | 0.780 | 8 | -3.0 | 0.24 | 5.951 | 0.669 | 2.951 | 0.712 | 9 | -2.0 | 0.24 | 7.610 | 0.728 | 5.610 | 0.767 | 10 | -1.0 | 0.24 | 9.210 | 0.751 | 8.210 | 0.789 | 11 | 0.0 | 0.24 | 10.80 | 0.836 | 10.80 | 0.870 | 12 | 0.0 | 0.24 | 10.90 | 0.821 | 10.90 | 0.856 | 13 | 1.0 | 0.24 | 13.05 | 0.802 | 14.05 | 0.838 | 14 | 2.0 | 0.24 | 14.47 | 0.869 | 16.47 | 0.902 | 15 | 2.0 | 0.24 | 14.44 | 0.874 | 16.44 | 0.907 |
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