International Journal of Aerospace Engineering / 2016 / Article / Tab 7

Research Article

Multiple Gravity Assist Spacecraft Trajectories Design Based on BFS and EP_DE Algorithm

Table 7

Feature vector matrix in GTOC1.
(a)

First componentSecond componentThird componentFourth componentFifth componentSixth componentSeventh componentEighth component

−0.3850−0.2518−0.25100.1105−0.34930.17040.24270.7093
−0.04920.31200.3859−0.6696−0.31990.4230−0.10610.1021
−0.27760.6459−0.5983−0.15800.29050.06220.1809−0.0423
0.48420.4185−0.12840.3069−0.6616−0.09480.1762−0.0452
−0.47230.39720.52640.2188−0.0206−0.52240.03460.1403
0.36600.0344−0.1872−0.37400.0992−0.5419−0.36160.5057
0.38560.04540.2862−0.07290.39090.04900.73120.2686
0.17940.29300.14000.47670.30080.4585−0.44660.3675

(b)

First componentSecond componentThird componentFourth componentFifth componentSixth componentSeventh componentEighth component

−0.12870.0755−0.57790.4540−0.10940.2181−0.1042−0.6060
−0.0511−0.03470.1628−0.4753−0.65510.50420.1035−0.2230
−0.0646−0.1284−0.0644−0.19910.59420.38440.6374−0.1686
0.06960.00400.0960−0.21240.42700.4605−0.7376−0.0494
−0.11240.0311−0.1876−0.62250.1176−0.5663−0.1099−0.4659
−0.0825−0.13450.75300.30880.0690−0.12010.0018−0.5418
0.79230.56440.0581−0.01580.02250.00720.1200−0.1873
0.5697−0.7994−0.14370.0071−0.0664−0.0574−0.0402−0.0799

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