Flight Control Laws Verification Using Continuous Genetic Algorithms

Table 7

Same as Table 6, but using a modified Sinc function.

Mach	Alt.	Run 1		Run 2		Run 3		Run 4		Max value
		Iter. no.	AOA	Iter. no.	AOA	Iter. no.	AOA	Iter. no.	AOA
0.3	1000	182	19.30103	170	19.04308	251	20.60302	166	19.00672	20.60302
0.6	6000	210	20.24026	207	20.67776	262	20.89506	208	19.15628	20.89506
0.8	3000	175	13.64315	239	21.17564	210	20.24026	207	20.67776	21.17564
1	5000	210	20.24026	207	20.67776	262	20.89506	209	18.92149	20.89506
1.2	3000	200	21.0805	364	14.64127	192	19.00408	255	12.94459	21.0805
1.2	6000	450	20.90201	257	12.77573	178	19.91921	181	15.52381	20.90201