An Accurate Method for Real-Time Aircraft Dynamics Simulation Based on Predictor-Corrector Scheme

Table 2

Numerical errors due to different values of the parameters in (13a), (13b), and (13c).

	Formula (13a)			Formula (13b)			Formula (13c)
	(FDM)			(QR)			(GA with a punishment strategy)
	0.0000
0.0200
0.0400
0.0600
0.0800
0.1000
0.1200
0.1400
0.1600
0.1800
0.2000