Research Article
Sinking Velocity Impact-Analysis for the Carrier-Based Aircraft Using the Response Surface Method-Based Improved Kriging Algorithm
Table 1
Partial correlation analysis results between deck landing parameters and sinking velocity of F/A-18A.
| | No. | Parameters | Correlation coefficient | Correlation degree |
| | 1 | Aircraft glide angle | 0.988 | Highly positive correlation | | 2 | Deck pitch angle | −0.890 | Highly negative correlation | | 3 | Engaging velocity | 0.561 | Moderately positive correlation | | 4 | Approach velocity | 0.545 | Moderately positive correlation | | 5 | Aircraft pitch rate | −0.225 | No | | 6 | Carrier velocity | 0.215 | No | | 7 | Landing weight | 0.196 | No | | 8 | Deck roll angle | −0.094 | No | | 9 | Aircraft roll angle | −0.093 | No | | 10 | Aircraft roll rate | −0.084 | No | | 11 | Aircraft pitch rate | −0.064 | No | | 12 | Aircraft pitch angle | 0.058 | No | | 13 | Aircraft yaw angle | −0.041 | No | | 14 | Ramp to touchdown distance | −0.041 | No | | 15 | Off-center engaging distance | −0.001 | No |
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