International Scholarly Research Notices / 2013 / Article / Fig 7

Research Article

Flight Control Laws Verification Using Continuous Genetic Algorithms

Figure 7

Maximum load factor versus the iteration (generation). Result using CGA with population sizes of 64 and 128 and both initialization functions: modified Gauss function and modified Sinc function . Aircraft model trimmed at 1000 m altitude and 0.3 Mach speed.
496457.fig.007

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