Aircraft Control Parameter Estimation Using Self-Adaptive Teaching-Learning-Based Optimization with an Acceptance Probability

Table 6

Hansa-3 aerodynamics coefficient simulated without noise, noise 5% and 10%.

True value		Without noise			Noise 5%			Noise 10%
		SaTLBO-AP	SaDE	WCA	SaTLBO-AP	SaDE	WCA	SaTLBO-AP	SaDE	WCA
	0.036	0.0367	0.0368	0.0437	0.038	0.0463	0.0544	0.0403	0.023	0
		(0.0079)	(0.0086)	(0.0253)	(0.009)	(0.0058)	(0.0227)	(0.0089)	(0.0076)	(0.0172)
	0.061	0.0587	0.0511	0.0183	0.0703	0.0433	0.0002	0.0368	0.1879	0.8955
		(0.0558)	(0.054)	(0.2957)	(0.0544)	(0.0456)	(0.273)	(0.0566)	(0.1109)	(0.3237)
	0.152	0.1454	0.1486	0.0972	0.1366	0.065	0	0.1611	0.2274	0
		(0.0532)	(0.0721)	(0.2322)	(0.0638)	(0.0511)	(0.2145)	(0.0698)	(0.0868)	(0.2046)
	0.23	0.2297	0.2302	0.2384	0.2333	0.2193	0.126	0.2416	0.2005	0.0001
		(0.0037)	(0.0077)	(0.1389)	(0.015)	(0.0173)	(0.1284)	(0.0178)	(0.0504)	(0.1133)
	4.886	4.9015	4.8831	4.938	5.053	5.1848	5.3335	4.846	4.1228	5.5128
		(0.0295)	(0.1079)	(0.814)	(0.066)	(0.0597)	(0.7129)	(0.1371)	(0.5722)	(1.0446)
	37.259	37.1573	37.281	34.3262	39.5509	41.9119	48.286	43.377	57.2311	87.3309
		(1.2757)	(2.1063)	(56.1791)	(2.9128)	(2.2761)	(37.4155)	(6.5266)	(12.6068)	(50.7457)
	0.376	0.3755	0.376	0.2488	0.1776	0.2639	1.2234	0.0033	1.0604	2.1766
		(0.0406)	(0.0672)	(1.2566)	(0.1403)	(0.1831)	(1.0458)	(0.1661)	(0.3744)	(0.9867)
	0.091	0.091	0.091	0.0906	0.0922	0.0944	0.0918	0.1035	0.0969	0.1037
		(0.0002)	(0.0008)	(0.0121)	(0.0005)	(0.001)	(0.0108)	(0.0009)	(0.0054)	(0.0392)
	−0.412	−0.4132	−0.4119	−0.4151	−0.4329	−0.4186	−0.4239	−0.4652	−0.3811	−0.517
		(0.0014)	(0.0037)	(0.1517)	(0.004)	(0.0082)	(0.0933)	(0.0118)	(0.0456)	(0.2)
	−8.792	−8.758	−8.8043	−8.6207	−8.6012	−8.8541	−8.1431	−10.2257	−10.221	−7.5769
		(0.0676)	(0.2355)	(3.3145)	(0.1825)	(0.3182)	(2.143)	(0.4649)	(1.3053)	(10.9678)
	−0.735	−0.7344	−0.7355	−0.7288	−0.73	−0.763	−0.7343	−0.8156	−0.8112	−0.7767
		(0.0019)	(0.0093)	(0.0954)	(0.0063)	(0.0093)	(0.073)	(0.0153)	(0.055)	(0.37)